IRIDIUM 33 DEB, 33886

Orbit data source: Space-Track

IRIDIUM 33 DEB, 33886 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
33886, 1997-051BF
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, 0.9 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

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

TLE from 12 hours ago
0 IRIDIUM 33 DEB
1 33886U 97051BF  26065.65114738  .00000882  00000-0  29575-3 0  9993
2 33886  86.3841  31.8841 0013313 341.1038 192.0703 14.36164324892562
Epoch: 2026-03-06T15:37Z
TLE epoch observation values (Epoch: 2026-03-06T15:37:39.133Z)
Latitude
6.76693°
Longitude
172.65961°
Altitude
782.939 km
Speed
7.458 km/s
True Right ascension
14h 05m 49s
True Declination
6° 43' 37"
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
07:11:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
777.676 km
Perigee altitude
758.648 km
Semi-major axis
7,146.299 km
Eccentricity
0.00133
Inclination
86.3841°
RAAN
31.8841°
Arg. of periapsis
341.1038°
True anomaly
192.03845°
Mean anomaly
192.0703°
Eccentric anomaly
192.05437°
Mean motion
3.5927 °/min
Orbital period
100.2 mins
BSTAR
0.00029575
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|