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IRIDIUM 28, 24948

Orbit data source: Space-Track

IRIDIUM 28, 24948 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.

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Identifier
24948, 1997-051E
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, 4.0 m
Radar Cross Section
5.666 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago
0 IRIDIUM 28
1 24948U 97051E   26038.04617776  .00000420  00000-0  13333-3 0  9998
2 24948  86.3927  42.6657 0002550  79.3142 280.8343 14.37610849487585
Epoch: 2026-02-07T01:06Z
TLE epoch observation values (Epoch: 2026-02-07T01:06:29.758Z)
Latitude
Longitude
-111.13362°
Altitude
769.117 km
Speed
7.47 km/s
True Right ascension
02h 50m 39s
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
15:38:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
765.184 km
Perigee altitude
761.542 km
Semi-major axis
7,141.5 km
Eccentricity
0.00026
Inclination
86.3927°
RAAN
42.6657°
Arg. of periapsis
79.3142°
True anomaly
280.8056°
Mean anomaly
280.8343°
Eccentric anomaly
280.81995°
Mean motion
3.59633 °/min
Orbital period
100.1 mins
BSTAR
0.00013333
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