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: 5 hours ago

TLE from 5 hours ago
0 IRIDIUM 33 DEB
1 33886U 97051BF  26064.15650062  .00000795  00000-0  26600-3 0  9991
2 33886  86.3838  32.5133 0013489 346.2781  24.1855 14.36161466892359
Epoch: 2026-03-05T03:45Z
TLE epoch observation values (Epoch: 2026-03-05T03:45:21.653Z)
Latitude
10.45154°
Longitude
173.92658°
Altitude
764.715 km
Speed
7.477 km/s
True Right ascension
02h 12m 42s
True Declination
10° 23' 26"
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
12:47:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
777.811 km
Perigee altitude
758.532 km
Semi-major axis
7,146.308 km
Eccentricity
0.00135
Inclination
86.3838°
RAAN
32.5133°
Arg. of periapsis
346.2781°
True anomaly
24.24892°
Mean anomaly
24.1855°
Eccentric anomaly
24.2172°
Mean motion
3.5927 °/min
Orbital period
100.2 mins
BSTAR
0.000266
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|