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GLOBALSTAR M022

NORAD 25649 Payload LEO 1999-012A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
1667 km
Apogee
1672 km
Inclination
52.0°
Period
119.8 min
Mean Motion
12.02513595 rev/day
TLE Epoch
2026-06-19 17:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,670 km
Orbital Velocity25,347 km/h
Velocity7.04 km/s
Orbital Period120 minutes
Orbits / Day12.03
Eccentricity0.0003
Semi-Major Axis8,041 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
Globalstar (Globalstar)
Launch Date
1999-03-15
Launch Site
Baikonur, Kazakhstan
Int'l Designator
1999-012A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
GLOBALSTAR M022 is an active satellite operated by Globalstar (Globalstar), launched on 1999-03-15 from Baikonur, Kazakhstan. With over 27 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 1,667 km and 1,672 km with an inclination of 52.0°. It travels at approximately 25,347 km/h (7.04 km/s), completing one full orbit every 120 minutes — that’s roughly 12.03 orbits per day. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is thousands of years. Orbital Radar tracks GLOBALSTAR M022 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
GLOBALSTAR M022 orbits at an average altitude of 1,670 km in the uppermost reaches of Low Earth Orbit. At this altitude, orbital decay is effectively zero without active deorbiting, and coverage footprints are significantly larger than lower LEO, though at the cost of higher latency. Within ±50 km of GLOBALSTAR M022’s average altitude, there are currently 19 active payloads and 88 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 52.0°, GLOBALSTAR M022 passes over latitudes between 52.0°N and 52.0°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. Globalstar operates approximately 84 active satellites in total, of which 10 share a similar altitude band with GLOBALSTAR M022.
🔗 Globalstar Constellation

This satellite is part of the Globalstar constellation, a LEO mobile satellite communications system providing voice, data and IoT services. The second-generation constellation operates 24 satellites at approximately 1,414 km altitude with a 52° inclination. Globalstar also provides the backbone for Apple's Emergency SOS via satellite feature on iPhones.

❓ Frequently Asked Questions
GLOBALSTAR M022 orbits in Low Earth Orbit (LEO) at altitudes between 1,667 km (perigee) and 1,672 km (apogee), with an average altitude of approximately 1,670 km. It completes one orbit every 120 minutes, travelling at approximately 25,347 km/h (15,750 mph).
GLOBALSTAR M022 is operated by Globalstar (Globalstar). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 25649. You can track GLOBALSTAR M022 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
GLOBALSTAR M022 was launched on 1999-03-15 from Baikonur, Kazakhstan, the world’s first and largest operational space launch facility, located in Kazakhstan. At its current altitude, the estimated remaining orbital lifetime is: thousands of years. View the full satellite launch log.
Yes — Orbital Radar tracks GLOBALSTAR M022 (NORAD ID 25649) 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.
GLOBALSTAR M022 travels at approximately 25,347 km/h (15,750 mph) — roughly 7.04 km/s. It completes 12.03 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 24 sunrises and sunsets every 24 hours.