COSMOS 158, 2801
Orbit data source: Space-Track
COSMOS 158, 2801 is a payload satellite owned by OKB-10 (CIS) in LEO that was launched on Mon, 15 May 1967 UTC via a KOSMOS 11K65M launch vehicle from the Plesetsk Missile And Space Complex (PKMTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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2801 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
OKB-10
Mission
Spacecraft
Bus & Motor
KAUR-1 11F617, Unknown motor
Mass
800 kg wet, 800 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 COSMOS 158
1 02801U 67045A 25309.49264389 .00000030 00000-0 18645-4 0 9998
2 02801 74.0378 116.2630 0056661 17.7916 342.5204 14.36908932 64292Epoch: 2025-11-05T11:49Z
TLE epoch observation values (Epoch: 2025-11-05T11:49:24.432Z)
Latitude
0.00007°
Longitude
-106.05331°
Altitude
732.731 km
Speed
7.509 km/s
True Right ascension
07h 45m 03s
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
17:28:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
806.834 km
Perigee altitude
725.871 km
Semi-major axis
7,144.489 km
Eccentricity
0.00567
Inclination
74.0378°
RAAN
116.263°
Arg. of periapsis
17.7916°
True anomaly
342.32405°
Mean anomaly
342.5204°
Eccentric anomaly
342.42236°
Mean motion
3.59407 °/min
Orbital period
100.17 mins
BSTAR
0.000018645
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Other satellites on launch #45 in the year 1967 (1967-05-15 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 158 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-11-06 21:47:37.457Z | 359.846° N | 2025-11-06 21:51:37.457Z | 57.258° ENE | 31.588° | 2025-11-06 21:56:37.457Z | 131.888° SE |
| 7 mins | 2025-11-06 23:30:37.457Z | 306.43° NW | 2025-11-06 23:33:37.457Z | 263.713° W | 23.328° | 2025-11-06 23:37:37.457Z | 210.318° SW |
| 8 mins | 2025-11-07 12:24:37.457Z | 206.82° SW | 2025-11-07 12:28:37.457Z | 305.163° NW | 43.531° | 2025-11-07 12:32:37.457Z | 13.498° NNE |
| 6 mins | 2025-11-07 21:12:37.457Z | 26.362° NE | 2025-11-07 21:14:37.457Z | 56.726° ENE | 21.828° | 2025-11-07 21:18:37.457Z | 109.786° ESE |
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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