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
Last TLE update
9 hours ago
Origin
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 (26 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, 6.0 m
Radar Cross Section
5.587 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 9 hours ago
0 GLOBALSTAR M023
1 25621U 99004A   25199.61783619 -.00000189  00000-0 -47363-3 0  9991
2 25621  52.0130 317.7352 0010134 191.4362 182.3120 12.62503736219792
Epoch: 2025-07-18T14:49Z
TLE epoch observation values (Epoch: 2025-07-18T14:49:41.046Z)
Latitude
10.78301°
Longitude
167.15819°
Altitude
1,420.453 km
Speed
7.149 km/s
True Right ascension
21h 44m 59s
True Declination
10° 43' 31"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
-43.42724°
Longitude
24.88389°
Altitude
1,421.908 km
Speed
7.153 km/s
Apparent Right ascension
11h 19m 07s
Apparent Declination
-85° 07' 47"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
12:25:05
Azimuth
181.691° SSW
Elevation
-35.234°
Doppler factor
1
Orbital elements
Apogee altitude
1,420.913 km
Perigee altitude
1,405.122 km
Semi-major axis
7,791.155 km
Eccentricity
0.00101
Inclination
52.013°
RAAN
317.7352°
Arg. of periapsis
191.4362°
True anomaly
182.30732°
Mean anomaly
182.312°
Eccentric anomaly
182.30966°
Mean motion
3.15602 °/min
Orbital period
114.07 mins
BSTAR
-0.00047363
Loading maneuver chart data...
Loading SW <> Apogee altitude chart data...
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)
|