COSMOS 2251 DEB, 34388
Orbit data source: Space-Track
COSMOS 2251 DEB, 34388 is space debris in LEO originally from a launch on Wed, 16 Jun 1993 UTC launched from the Plesetsk Missile And Space Complex (PKMTR). 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.
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34388 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 COSMOS 2251 DEB
1 34388U 93036QD 26034.31724284 .00003010 00000-0 78746-3 0 9992
2 34388 74.0401 124.4718 0011620 170.2933 246.5973 14.49746178889176Epoch: 2026-02-03T07:36Z
TLE epoch observation values (Epoch: 2026-02-03T07:36:49.781Z)
Latitude
53.64429°
Longitude
-100.50146°
Altitude
738.215 km
Speed
7.489 km/s
True Right ascension
09h 48m 49s
True Declination
53° 28' 46"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
04:47:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
732.339 km
Perigee altitude
715.833 km
Semi-major axis
7,102.223 km
Eccentricity
0.00116
Inclination
74.0401°
RAAN
124.4718°
Arg. of periapsis
170.2933°
True anomaly
246.47517°
Mean anomaly
246.5973°
Eccentric anomaly
246.53623°
Mean motion
3.6262 °/min
Orbital period
99.28 mins
BSTAR
0.00078746
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Other satellites on launch #36 in the year 1993 (1993-06-16 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.COSMOS 2251 DEB Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-02-04 06:39:30.550Z | 176.079° S | 2026-02-04 06:43:30.550Z | 103.392° ESE | 38.046° | 2026-02-04 06:47:30.550Z | 32.02° NE |
| 5 mins | 2026-02-04 08:22:30.550Z | 267.383° W | 2026-02-04 08:24:30.550Z | 294.491° NW | 17.587° | 2026-02-04 08:27:30.550Z | 336.767° NNW |
| 7 mins | 2026-02-04 17:03:30.550Z | 346.517° N | 2026-02-04 17:06:30.550Z | 68.739° E | 44.415° | 2026-02-04 17:10:30.550Z | 156.749° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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