Showing default

GLOBALSTAR M028, 25875

Orbit data source: Space-Track

GLOBALSTAR M028, 25875 is a payload satellite owned by Globalstar (US) in LEO that was launched on Sun, 25 Jul 1999 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
25875, 1999-041D
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)
1999-07-25 (27 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: 18 hours ago

TLE from 18 hours ago
0 GLOBALSTAR M028
1 25875U 99041D   26031.81490886 -.00000060  00000-0  26097-3 0  9990
2 25875  51.9600 231.3299 0062783 207.2513 152.5048 12.50595537218788
Epoch: 2026-01-31T19:33Z
TLE epoch observation values (Epoch: 2026-01-31T19:33:28.125Z)
Latitude
-0.00001°
Longitude
166.92921°
Altitude
1,506.406 km
Speed
7.093 km/s
True Right ascension
15h 25m 19s
True Declination
0° 00' 00"
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
15:27:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,511.626 km
Perigee altitude
1,413.175 km
Semi-major axis
7,840.538 km
Eccentricity
0.00628
Inclination
51.96°
RAAN
231.3299°
Arg. of periapsis
207.2513°
True anomaly
152.83465°
Mean anomaly
152.5048°
Eccentric anomaly
152.66995°
Mean motion
3.12626 °/min
Orbital period
115.15 mins
BSTAR
0.00026097
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 #41 in the year 1999 (1999-07-25 UTC)

Documentation

Showing up to 5 results
|