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GLOBALSTAR M040, 25622

Orbit data source: Space-Track

GLOBALSTAR M040, 25622 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.

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Identifier
25622, 1999-004B
Orbit
LEO
Country
Flag of UnknownUnknown / 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 (27 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
Last TLE update: 14 hours ago

TLE from 14 hours ago
0 GLOBALSTAR M040
1 25622U 99004B   25291.31992304 -.00000053  00000-0  28443-3 0  9992
2 25622  51.9937  42.8317 0000179 347.1600  31.4945 12.62019608230800
Epoch: 2025-10-18T07:40Z
TLE epoch observation values (Epoch: 2025-10-18T07:40:41.350Z)
Latitude
14.61033°
Longitude
-87.69832°
Altitude
1,414.479 km
Speed
7.155 km/s
True Right ascension
03h 38m 06s
True Declination
14° 32' 01"
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
16:11:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,415.152 km
Perigee altitude
1,414.873 km
Semi-major axis
7,793.15 km
Eccentricity
0.00002
Inclination
51.9937°
RAAN
42.8317°
Arg. of periapsis
347.16°
True anomaly
31.49557°
Mean anomaly
31.4945°
Eccentric anomaly
31.49504°
Mean motion
3.15481 °/min
Orbital period
114.11 mins
BSTAR
0.00028443
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Other satellites on launch #4 in the year 1999 (1999-02-09 UTC)

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