IRIDIUM 33 DEB, 33870

Orbit data source: Space-Track

IRIDIUM 33 DEB, 33870 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
33870, 1997-051AP
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: 8 hours ago

TLE from 8 hours ago
0 IRIDIUM 33 DEB
1 33870U 97051AP  26090.20066836  .00003191  00000-0  87917-3 0  9990
2 33870  86.3800  11.7444 0020164 176.0455 345.3463 14.46517901897044
Epoch: 2026-03-31T04:48Z
TLE epoch observation values (Epoch: 2026-03-31T04:48:57.746Z)
Latitude
18.62234°
Longitude
-70.29247°
Altitude
725.709 km
Speed
7.501 km/s
True Right ascension
12h 42m 07s
True Declination
18° 31' 05"
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
18:00:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
748.333 km
Perigee altitude
719.651 km
Semi-major axis
7,112.129 km
Eccentricity
0.00202
Inclination
86.38°
RAAN
11.7444°
Arg. of periapsis
176.0455°
True anomaly
345.2877°
Mean anomaly
345.3463°
Eccentric anomaly
345.31702°
Mean motion
3.61863 °/min
Orbital period
99.49 mins
BSTAR
0.00087917
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|