IRIDIUM 33 DEB, 35628

Orbit data source: Space-Track

IRIDIUM 33 DEB, 35628 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
35628, 1997-051RA
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, 0.1 m
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 IRIDIUM 33 DEB
1 35628U 97051RA  26036.58274948  .00015558  00000-0  26629-2 0  9991
2 35628  86.3603 344.6003 0012904 129.7673 230.4680 14.68688354872512
Epoch: 2026-02-05T13:59Z
TLE epoch observation values (Epoch: 2026-02-05T13:59:09.555Z)
Latitude
-0.00007°
Longitude
-0.92242°
Altitude
674.151 km
Speed
7.517 km/s
True Right ascension
22h 58m 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
09:39:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
671.26 km
Perigee altitude
653.09 km
Semi-major axis
7,040.312 km
Eccentricity
0.00129
Inclination
86.3603°
RAAN
344.6003°
Arg. of periapsis
129.7673°
True anomaly
230.35407°
Mean anomaly
230.468°
Eccentric anomaly
230.41102°
Mean motion
3.67414 °/min
Orbital period
97.98 mins
BSTAR
0.0026629
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|