Skip to content
Home Library Satellite Directory NTS 2 AKM

NTS 2 AKM

NORAD 26376 Rocket Body MEO 1977-053C
CONNECTING… MEO · NORAD 26376
NOW PASSING OVER
Calculating position…
Altitude (km)
Speed (km/s)
Latitude
Longitude
Real-time tracking powered by Orbital Radar
ORBITAL RADAR · LIVE GROUND TRACK
🌍 Track on 3D Globe
🛰️ Orbital Parameters
Perigee
18740 km
Apogee
20979 km
Inclination
62.8°
Period
704.9 min
Mean Motion
2.04277332 rev/day
TLE Epoch
2026-06-23 01:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude19,860 km
Orbital Velocity14,034 km/h
Velocity3.90 km/s
Orbital Period11 hours 45 minutes
Orbits / Day2.04
Eccentricity0.0427
Semi-Major Axis26,231 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1977-06-23
Launch Site
Vandenberg SFB, California
Int'l Designator
1977-053C
Object Type
Rocket Body
RCS Size
Medium (0.1–1 m²)
📖 About This Object
NTS 2 AKM is a spent rocket body associated with United States, launched on 1977-06-23 from Vandenberg SFB, California on the NTS 2 launch. With over 49 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 18,740 km and 20,979 km with an inclination of 62.8°. It travels at approximately 14,034 km/h (3.90 km/s), completing one full orbit every 11 hours 45 minutes — that’s roughly 2.04 orbits per day. Spent rocket bodies like NTS 2 AKM are among the largest pieces of uncontrolled space debris and are priority targets for collision avoidance manoeuvres and future active debris removal efforts.
🌍 Orbit Context
NTS 2 AKM orbits at an average altitude of 19,860 km in Medium Earth Orbit, the region between LEO and GEO (2,000–35,786 km). MEO’s higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer spacecraft are needed for global coverage — but signal latency is higher and radiation from the Van Allen belts is a significant design constraint. Within ±50 km of NTS 2 AKM’s average altitude, there are currently 1 active payload and 26 tracked debris or rocket body fragments. This is a relatively sparse altitude band, containing less than 1% of all active satellites. With an inclination of 62.8°, NTS 2 AKM passes over latitudes between 62.8°N and 62.8°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. United States operates approximately 12,413 active satellites in total.
🔗 Spent Rocket Body

This is a spent rocket body — the upper stage of a launch vehicle that remains in orbit after delivering its payload. Rocket bodies are a significant contributor to the space debris population. Older stages often retained residual propellant that could later explode, creating debris fields. Modern guidelines require upper stages to either deorbit (controlled re-entry) or passivate (vent residual fuel) to reduce fragmentation risk. The FCC's 5-year deorbit rule and UN debris mitigation guidelines are increasingly enforced to address this growing problem.

❓ Frequently Asked Questions
NTS 2 AKM orbits in Medium Earth Orbit (MEO) at altitudes between 18,740 km (perigee) and 20,979 km (apogee), with an average altitude of approximately 19,860 km. It completes one orbit every 11 hours 45 minutes, travelling at approximately 14,034 km/h (8,720 mph).
NTS 2 AKM (NORAD ID 26376) is a spent rocket body — the upper stage of a launch vehicle attributed to United States. It no longer serves a functional purpose but continues to orbit Earth as tracked debris. Spent upper stages are among the largest uncontrolled objects in orbit and are closely monitored for collision risk.
NTS 2 AKM was launched on 1977-06-23 from Vandenberg SFB, California, primarily used for polar and sun-synchronous orbit launches due to its southward ocean trajectory from California. View the full satellite launch log.
Yes — Orbital Radar tracks NTS 2 AKM (NORAD ID 26376) using the latest TLE (two-line element set) data from Space-Track and CelesTrak. Open the live tracker to see its current position, altitude, speed and orbital path updated in real time. You can also browse the satellite directory to find other tracked objects.
NTS 2 AKM travels at approximately 14,034 km/h (8,720 mph) — roughly 3.90 km/s. It completes 2.04 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 4 sunrises and sunsets every 24 hours.