GLOBALSTAR M060
NORAD 26083
Payload
LEO
2000-008C
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LEO · NORAD 26083
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Altitude (km)
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Speed (km/s)
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Longitude
🛰️ Orbital Parameters
Perigee
1600 km
Apogee
1605 km
Inclination
52.0°
Period
118.3 min
Mean Motion
12.17679003 rev/day
TLE Epoch
2026-06-19 03:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,603 km
Orbital Velocity25,453 km/h
Velocity7.07 km/s
Orbital Period118 minutes
Orbits / Day12.18
Eccentricity0.0003
Semi-Major Axis7,974 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
Globalstar (Globalstar)
Launch Date
2000-02-08
Launch Site
Cape Canaveral, Florida
Int'l Designator
2000-008C
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
GLOBALSTAR M060 is an active satellite operated by Globalstar (Globalstar), launched on 2000-02-08 from Cape Canaveral, Florida. With over 26 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 1,600 km and 1,605 km with an inclination of 52.0°. It travels at approximately 25,453 km/h (7.07 km/s), completing one full orbit every 118 minutes — that’s roughly 12.18 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 M060 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 M060 orbits at an average altitude of 1,603 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 M060’s average altitude, there are currently 29 active payloads and 193 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 M060 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 12 share a similar altitude band with GLOBALSTAR M060.
🔗 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 M060 orbits in Low Earth Orbit (LEO) at altitudes between 1,600 km (perigee) and 1,605 km (apogee), with an average altitude of approximately 1,603 km. It completes one orbit every 118 minutes, travelling at approximately 25,453 km/h (15,816 mph).
GLOBALSTAR M060 is operated by Globalstar (Globalstar). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 26083. You can track GLOBALSTAR M060 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
GLOBALSTAR M060 was launched on 2000-02-08 from Cape Canaveral, Florida, one of the busiest launch facilities in the world, operated by NASA and the U.S. Space Force on Florida’s Atlantic coast. At its current altitude, the estimated remaining orbital lifetime is: thousands of years. View the full satellite launch log.
Yes — Orbital Radar tracks GLOBALSTAR M060 (NORAD ID 26083) 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 M060 travels at approximately 25,453 km/h (15,816 mph) — roughly 7.07 km/s. It completes 12.18 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 24 sunrises and sunsets every 24 hours.