Showing default

GLOBALSTAR M087, 52888

Orbit data source: Space-Track

GLOBALSTAR M087, 52888 is a payload satellite owned by Globalstar (US) in LEO that was launched on Sun, 19 Jun 2022 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

Loading next visibility...
Identifier
52888, 2022-064A
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
Thales Alenia
Mission
Operational Commercial Communications
Bus & Motor
PRISMA?, LS-400 AOCS?
Mass
715 kg wet, ~500 kg dry
Launch date (UTC)
2022-06-19 (3 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 6.0 m
Radar Cross Section
28.800 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 17 hours ago

TLE from 17 hours ago
0 GLOBALSTAR M087
1 52888U 22064A   25311.92199639 -.00000082  00000-0  12195-3 0  9997
2 52888  52.0022  16.0815 0000499 139.6230 220.4674 12.62260170163193
Epoch: 2025-11-07T22:07Z
TLE epoch observation values (Epoch: 2025-11-07T22:07:40.488Z)
Latitude
0.00001°
Longitude
-3.19621°
Altitude
1,414.607 km
Speed
7.154 km/s
True Right ascension
01h 04m 19s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
11:22:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,414.41 km
Perigee altitude
1,413.633 km
Semi-major axis
7,792.158 km
Eccentricity
0.00005
Inclination
52.0022°
RAAN
16.0815°
Arg. of periapsis
139.623°
True anomaly
220.46369°
Mean anomaly
220.4674°
Eccentric anomaly
220.46554°
Mean motion
3.15542 °/min
Orbital period
114.09 mins
BSTAR
0.00012195
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Other satellites on launch #64 in the year 2022 (2022-06-19 UTC)

Documentation

Showing up to 5 results
|