Showing default

GLOBALSTAR M023, 25621

Orbit data source: Space-Track

GLOBALSTAR M023, 25621 is a payload satellite owned by Globalstar (US) in LEO that was launched on Tue, 09 Feb 1999 UTC via a SOYUZ-U-PVB launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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
25621, 1999-004A
Orbit
LEO
Country
Flag of USUS / GLOB
Related business
Manufacturer
SS/Loral
Mission
Non-operational Commercial Communications
Bus & Motor
LS-400, LS-400 AOCS
Mass
450 kg wet, 380 kg dry
Launch date (UTC)
1999-02-09 (28 years ago)
Launch vehicle
SOYUZ-U-PVB
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 6.3 m
Radar Cross Section
5.587 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 8 hours ago

TLE from 8 hours ago
0 GLOBALSTAR M023
1 25621U 99004A   26271.18657247 -.00000071  00000-0  18080-3 0  9995
2 25621  52.0101  68.3291 0010609  82.6541  88.7692 12.62535533274848
Epoch: 2026-09-28T04:28Z
TLE epoch observation values (Epoch: 2026-09-28T04:28:39.861Z)
Latitude
6.62251°
Longitude
169.01674°
Altitude
1,412.398 km
Speed
7.156 km/s
True Right ascension
16h 12m 36s
True Declination
6° 35' 12"
Sunlit
Object was in daylight 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
05:27:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,421.153 km
Perigee altitude
1,404.622 km
Semi-major axis
7,791.024 km
Eccentricity
0.00106
Inclination
52.0101°
RAAN
68.3291°
Arg. of periapsis
82.6541°
True anomaly
88.89075°
Mean anomaly
88.7692°
Eccentric anomaly
88.82997°
Mean motion
3.1561 °/min
Orbital period
114.06 mins
BSTAR
0.0001808
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 #4 in the year 1999 (1999-02-09 UTC)

Documentation

Showing up to 5 results
|