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GLOBALSTAR M044

NORAD 25678 Payload LEO 1999-019C ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
1720 km
Apogee
1730 km
Inclination
52.0°
Period
121.0 min
Mean Motion
11.90263803 rev/day
TLE Epoch
2026-06-19 14:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,725 km
Orbital Velocity25,260 km/h
Velocity7.02 km/s
Orbital Period2 hours 1 minutes
Orbits / Day11.90
Eccentricity0.0006
Semi-Major Axis8,096 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
Globalstar (Globalstar)
Launch Date
1999-04-15
Launch Site
Baikonur, Kazakhstan
Int'l Designator
1999-019C
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
GLOBALSTAR M044 is an active satellite operated by Globalstar (Globalstar), launched on 1999-04-15 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 1,720 km and 1,730 km with an inclination of 52.0°. It travels at approximately 25,260 km/h (7.02 km/s), completing one full orbit every 2 hours 1 minutes — that’s roughly 11.90 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 M044 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 M044 orbits at an average altitude of 1,725 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 M044’s average altitude, there are currently 14 active payloads and 44 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 M044 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 M044.
🔗 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 M044 orbits in Low Earth Orbit (LEO) at altitudes between 1,720 km (perigee) and 1,730 km (apogee), with an average altitude of approximately 1,725 km. It completes one orbit every 2 hours 1 minutes, travelling at approximately 25,260 km/h (15,696 mph).
GLOBALSTAR M044 is operated by Globalstar (Globalstar). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 25678. You can track GLOBALSTAR M044 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
GLOBALSTAR M044 was launched on 1999-04-15 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 M044 (NORAD ID 25678) 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 M044 travels at approximately 25,260 km/h (15,696 mph) — roughly 7.02 km/s. It completes 11.90 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 24 sunrises and sunsets every 24 hours.