IRIDIUM 33 DEB, 33866

Orbit data source: Space-Track

IRIDIUM 33 DEB, 33866 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
33866, 1997-051AK
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, 0.2 m
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 7 hours ago

TLE from 7 hours ago
0 IRIDIUM 33 DEB
1 33866U 97051AK  26038.07146471  .00003408  00000-0  13419-2 0  9992
2 33866  86.2971  69.1898 0112452 342.1164  45.7348 14.25548335876134
Epoch: 2026-02-07T01:42Z
TLE epoch observation values (Epoch: 2026-02-07T01:42:54.550Z)
Latitude
28.76274°
Longitude
-91.71282°
Altitude
754.391 km
Speed
7.509 km/s
True Right ascension
04h 44m 51s
True Declination
28° 37' 04"
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
10:40:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
884.388 km
Perigee altitude
722.867 km
Semi-major axis
7,181.765 km
Eccentricity
0.01125
Inclination
86.2971°
RAAN
69.1898°
Arg. of periapsis
342.1164°
True anomaly
46.66669°
Mean anomaly
45.7348°
Eccentric anomaly
46.19983°
Mean motion
3.56612 °/min
Orbital period
100.95 mins
BSTAR
0.0013419
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|