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: 2 days ago
TLE from 2 days ago
0 COSMOS 158
1 02801U 67045A 26170.96941695 .00000009 00000-0 11933-4 0 9998
2 02801 74.0408 59.9575 0058106 267.0345 92.4158 14.36941703 96825Epoch: 2026-06-19T23:15Z
TLE epoch observation values (Epoch: 2026-06-19T23:15:57.624Z)
Latitude
-0.00001°
Longitude
162.77663°
Altitude
773.225 km
Speed
7.467 km/s
True Right ascension
03h 59m 49s
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
14:33:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
807.757 km
Perigee altitude
724.73 km
Semi-major axis
7,144.38 km
Eccentricity
0.00581
Inclination
74.0408°
RAAN
59.9575°
Arg. of periapsis
267.0345°
True anomaly
93.08084°
Mean anomaly
92.4158°
Eccentric anomaly
92.74834°
Mean motion
3.59415 °/min
Orbital period
100.16 mins
BSTAR
0.000011933
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-06-22 03:37:12.743Z | 342.899° N | 2026-06-22 03:42:12.743Z | 23.54° NE | 44.354° | 2026-06-22 03:47:12.743Z | 158.714° S |
| 7 mins | 2026-06-22 16:34:12.743Z | 141.518° SSE | 2026-06-22 16:37:12.743Z | 91.633° ESE | 25.346° | 2026-06-22 16:41:12.743Z | 42.533° NE |
| 8 mins | 2026-06-22 18:15:12.743Z | 238.967° WSW | 2026-06-22 18:19:12.743Z | 307.246° NW | 29.596° | 2026-06-22 18:23:12.743Z | 359.454° N |
| 8 mins | 2026-06-23 03:02:12.743Z | 1.08° NNE | 2026-06-23 03:05:12.743Z | 54.782° ENE | 36.347° | 2026-06-23 03:10:12.743Z | 139.444° 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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