IRIDIUM 33 DEB, 46972

Orbit data source: Space-Track

IRIDIUM 33 DEB, 46972 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
46972, 1997-051ACE
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
1997-09-14 (28 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: 3 days ago

TLE from 3 days ago
0 IRIDIUM 33 DEB
1 46972U 97051ACE 26035.22156457  .00002948  00000-0  74102-3 0  9998
2 46972  86.3887  16.3705 0007168 296.9315 122.4772 14.50973059623480
Epoch: 2026-02-04T05:19Z
TLE epoch observation values (Epoch: 2026-02-04T05:19:03.178Z)
Latitude
59.38131°
Longitude
168.30468°
Altitude
735.374 km
Speed
7.491 km/s
True Right ascension
01h 29m 50s
True Declination
59° 13' 48"
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
08:00:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
724.501 km
Perigee altitude
714.326 km
Semi-major axis
7,097.55 km
Eccentricity
0.00072
Inclination
86.3887°
RAAN
16.3705°
Arg. of periapsis
296.9315°
True anomaly
122.54646°
Mean anomaly
122.4772°
Eccentric anomaly
122.51183°
Mean motion
3.62978 °/min
Orbital period
99.18 mins
BSTAR
0.00074102
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|