Showing default

IRIDIUM 29, 24944

Orbit data source: Space-Track

IRIDIUM 29, 24944 is a payload satellite owned by Iridium (US) in LEO that was launched on Sun, 14 Sep 1997 UTC via a PROTON-K/17S40 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
24944, 1997-051A
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
MOTO/LMMS
Mission
Non-operational Commercial Communications
Bus & Motor
LM700, Unknown motor
Mass
662 kg wet, 556 kg dry
Launch date (UTC)
1997-09-14 (28 years ago)
Launch vehicle
PROTON-K/17S40
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 4.2 m
Radar Cross Section
5.666 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 23 hours ago

TLE from 23 hours ago
0 IRIDIUM 29
1 24944U 97051A   25260.92302532  .00000369  00000-0  11887-3 0  9992
2 24944  86.3907 104.9942 0002070  82.7762 277.3671 14.36535182466588
Epoch: 2025-09-17T22:09Z
TLE epoch observation values (Epoch: 2025-09-17T22:09:09.387Z)
Latitude
0.00003°
Longitude
135.61307°
Altitude
772.834 km
Speed
7.468 km/s
True Right ascension
06h 59m 58s
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
14:25:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
768.41 km
Perigee altitude
765.452 km
Semi-major axis
7,145.068 km
Eccentricity
0.00021
Inclination
86.3907°
RAAN
104.9942°
Arg. of periapsis
82.7762°
True anomaly
277.34357°
Mean anomaly
277.3671°
Eccentric anomaly
277.35534°
Mean motion
3.59363 °/min
Orbital period
100.18 mins
BSTAR
0.00011887
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|