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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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 26081.85544786 .00000046 00000-0 23828-4 0 9994
2 02801 74.0396 223.7620 0055838 92.7379 268.0167 14.36932418 84025Epoch: 2026-03-22T20:31Z
TLE epoch observation values (Epoch: 2026-03-22T20:31:50.695Z)
Latitude
-0.00004°
Longitude
95.44494°
Altitude
772.868 km
Speed
7.467 km/s
True Right ascension
14h 55m 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
09:00:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
806.167 km
Perigee altitude
726.381 km
Semi-major axis
7,144.411 km
Eccentricity
0.00558
Inclination
74.0396°
RAAN
223.762°
Arg. of periapsis
92.7379°
True anomaly
267.37739°
Mean anomaly
268.0167°
Eccentric anomaly
267.69703°
Mean motion
3.59413 °/min
Orbital period
100.16 mins
BSTAR
0.000023828
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-03-24 09:24:58.050Z | 143.105° SSE | 2026-03-24 09:27:58.050Z | 102.847° ESE | 20.701° | 2026-03-24 09:31:58.050Z | 49.229° ENE |
| 7 mins | 2026-03-24 11:06:58.050Z | 236.042° WSW | 2026-03-24 11:09:58.050Z | 293.224° NW | 32.358° | 2026-03-24 11:13:58.050Z | 359.907° N |
| 8 mins | 2026-03-24 19:52:58.050Z | 5.039° NNE | 2026-03-24 19:55:58.050Z | 55.798° ENE | 31.511° | 2026-03-24 20:00:58.050Z | 133.404° SE |
| 6 mins | 2026-03-24 21:35:58.050Z | 295.207° NW | 2026-03-24 21:37:58.050Z | 263.827° W | 21.319° | 2026-03-24 21:41:58.050Z | 211.164° SW |
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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