IRIDIUM 33 DEB, 36483

Orbit data source: Space-Track

IRIDIUM 33 DEB, 36483 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
36483, 1997-051VZ
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: 2 weeks ago

TLE from 2 weeks ago
0 IRIDIUM 33 DEB
1 36483U 97051VZ  26143.81119606  .00000994  00000-0  27137-3 0  9999
2 36483  86.3798 343.1026 0007706 323.6335  36.4343 14.46407292674886
Epoch: 2026-05-23T19:28Z
TLE epoch observation values (Epoch: 2026-05-23T19:28:07.339Z)
Latitude
-0.00003°
Longitude
169.64968°
Altitude
736.064 km
Speed
7.489 km/s
True Right ascension
22h 52m 24s
True Declination
0° 00' 00"
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
00:14:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
739.835 km
Perigee altitude
728.874 km
Semi-major axis
7,112.492 km
Eccentricity
0.00077
Inclination
86.3798°
RAAN
343.1026°
Arg. of periapsis
323.6335°
True anomaly
36.48678°
Mean anomaly
36.4343°
Eccentric anomaly
36.46054°
Mean motion
3.61835 °/min
Orbital period
99.49 mins
BSTAR
0.00027137
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|