Showing default

GLOBALSTAR M003, 25165

Orbit data source: Space-Track

GLOBALSTAR M003, 25165 is a payload satellite owned by Globalstar (US) in LEO that was launched on Sat, 14 Feb 1998 UTC via a DELTA 7420-10C 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
25165, 1998-008D
Orbit
LEO
Country
Flag of UnknownUnknown / GLOB
Related business
Manufacturer
SS/Loral
Mission
Non-operational Commercial Communications
Bus & Motor
LS-400, Unknown motor
Mass
450 kg wet, 380 kg dry
Launch date (UTC)
1998-02-14 (28 years ago)
Launch vehicle
DELTA 7420-10C
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
5.587 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 4 hours ago

TLE from 4 hours ago
0 GLOBALSTAR M003
1 25165U 98008D   26038.63688554 -.00000189  00000-0 -10653-2 0  9995
2 25165  51.9849 236.3836 0008927  49.8502 340.5981 12.12029904261775
Epoch: 2026-02-07T15:17Z
TLE epoch observation values (Epoch: 2026-02-07T15:17:06.910Z)
Latitude
23.56145°
Longitude
-110.82158°
Altitude
1,621.354 km
Speed
7.066 km/s
True Right ascension
17h 04m 51s
True Declination
23° 26' 57"
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
21:57:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,634.977 km
Perigee altitude
1,620.683 km
Semi-major axis
8,005.967 km
Eccentricity
0.00089
Inclination
51.9849°
RAAN
236.3836°
Arg. of periapsis
49.8502°
True anomaly
340.56408°
Mean anomaly
340.5981°
Eccentric anomaly
340.58109°
Mean motion
3.02986 °/min
Orbital period
118.82 mins
BSTAR
-0.0010653
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...

Documentation

Showing up to 5 results
|