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: 7 hours ago

TLE from 7 hours ago
0 IRIDIUM 33 DEB
1 33886U 97051BF  26008.21825940  .00000584  00000-0  19389-3 0  9997
2 33886  86.3805  56.0798 0015053 152.7442 277.4341 14.36087775884325
Epoch: 2026-01-08T05:14Z
TLE epoch observation values (Epoch: 2026-01-08T05:14:17.612Z)
Latitude
69.77008°
Longitude
-120.43851°
Altitude
782.222 km
Speed
7.47 km/s
True Right ascension
04h 23m 38s
True Declination
69° 39' 31"
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
12:38:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
779.174 km
Perigee altitude
757.658 km
Semi-major axis
7,146.553 km
Eccentricity
0.00151
Inclination
86.3805°
RAAN
56.0798°
Arg. of periapsis
152.7442°
True anomaly
277.26301°
Mean anomaly
277.4341°
Eccentric anomaly
277.34856°
Mean motion
3.59251 °/min
Orbital period
100.21 mins
BSTAR
0.00019389
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|