IRIDIUM 33 DEB, 46971

Orbit data source: Space-Track

IRIDIUM 33 DEB, 46971 is space debris in LEO originally from a launch on Sun, 14 Sep 1997 UTC launched from the Tyuratam Missile And Space Complex (TTMTR). The debris from Iridium 33, an American commercial communications satellite, has been tracked extensively since its accidental collision with the defunct Russian satellite Cosmos 2251 in 2009. This event, occurring at high speed in low Earth orbit (LEO), generated thousands of pieces of space debris, significantly increasing the risk of further collisions. The Iridium 33 debris cloud has impacted space traffic management and orbital debris mitigation strategies, making it a subject of ongoing study in space situational awareness.

Loading next visibility...
Identifier
46971, 1997-051ACD
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
1997-09-14 (29 years ago)
Launch vehicle
Unknown
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 1 week ago

TLE from 1 week ago
0 IRIDIUM 33 DEB
1 46971U 97051ACD 26162.49650385  .00039423  00000-0  23538-2 0  9990
2 46971  86.3141 246.9992 0002667  51.4984 324.3215 15.10943599669484
Epoch: 2026-06-11T11:54Z
TLE epoch observation values (Epoch: 2026-06-11T11:54:57.932Z)
Latitude
15.74544°
Longitude
169.45335°
Altitude
534.294 km
Speed
7.598 km/s
True Right ascension
16h 32m 08s
True Declination
15° 39' 11"
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
08:41:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
532.022 km
Perigee altitude
528.337 km
Semi-major axis
6,908.317 km
Eccentricity
0.00027
Inclination
86.3141°
RAAN
246.9992°
Arg. of periapsis
51.4984°
True anomaly
324.30367°
Mean anomaly
324.3215°
Eccentric anomaly
324.31259°
Mean motion
3.77994 °/min
Orbital period
95.24 mins
BSTAR
0.0023538
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|