COSMOS 2251 DEB, 35888
Orbit data source: Space-Track
COSMOS 2251 DEB, 35888 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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35888 intel report (Beta)
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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: 1 day ago
TLE from 1 day ago
0 COSMOS 2251 DEB
1 35888U 93036AUB 26144.45620292 .00001094 00000-0 23585-3 0 9990
2 35888 74.0333 46.7624 0049415 137.9776 222.5197 14.58927874886461Epoch: 2026-05-24T10:56Z
TLE epoch observation values (Epoch: 2026-05-24T10:56:55.932Z)
Latitude
-0.00001°
Longitude
0.47126°
Altitude
725.127 km
Speed
7.479 km/s
True Right ascension
03h 07m 02s
True Declination
0° 00' 00"
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
21:43:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
729.185 km
Perigee altitude
659.289 km
Semi-major axis
7,072.374 km
Eccentricity
0.00494
Inclination
74.0333°
RAAN
46.7624°
Arg. of periapsis
137.9776°
True anomaly
222.13874°
Mean anomaly
222.5197°
Eccentric anomaly
222.32905°
Mean motion
3.64918 °/min
Orbital period
98.65 mins
BSTAR
0.00023585
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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 | 2026-05-25 18:20:14.293Z | 184.765° SSW | 2026-05-25 18:24:14.293Z | 111.823° ESE | 41.932° | 2026-05-25 18:28:14.293Z | 27.103° NE |
| 7 mins | 2026-05-26 04:40:14.293Z | 341.847° N | 2026-05-26 04:43:14.293Z | 68.086° E | 44.993° | 2026-05-26 04:47:14.293Z | 161.871° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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