COSMOS 2216, 22187
Orbit data source: Space-Track
COSMOS 2216, 22187 is a payload satellite owned by VKS (CIS) in LEO that was launched on Tue, 20 Oct 1992 UTC via a TSIKLON-3 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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22187 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
NPO PM
Mission
Defense Communications
Bus & Motor
STRELA-3, Unknown motor
Mass
225 kg wet, 225 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl, 0.8 m
Radar Cross Section
1.257 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 COSMOS 2216
1 22187U 92068F 26036.08839361 .00000023 00000-0 66780-4 0 9996
2 22187 82.5918 67.9760 0006540 81.3552 278.8280 12.62582558534224Epoch: 2026-02-05T02:07Z
TLE epoch observation values (Epoch: 2026-02-05T02:07:17.207Z)
Latitude
-0.00004°
Longitude
-99.09134°
Altitude
1,414.255 km
Speed
7.154 km/s
True Right ascension
04h 31m 54s
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
15:19:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,414.716 km
Perigee altitude
1,404.53 km
Semi-major axis
7,787.76 km
Eccentricity
0.00065
Inclination
82.5918°
RAAN
67.976°
Arg. of periapsis
81.3552°
True anomaly
278.75394°
Mean anomaly
278.828°
Eccentric anomaly
278.79097°
Mean motion
3.15809 °/min
Orbital period
113.99 mins
BSTAR
0.00006678
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Other satellites on launch #68 in the year 1992 (1992-10-20 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 2216 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. |
|---|---|---|---|---|---|---|---|
| 16 mins | 2026-02-05 14:08:06.507Z | 349.175° N | 2026-02-05 14:16:06.507Z | 272.979° WNW | 44.188° | 2026-02-05 14:24:06.507Z | 182.285° SSW |
| 4 mins | 2026-02-05 16:08:06.507Z | 296.504° NW | 2026-02-05 16:10:06.507Z | 281.421° WNW | 12.359° | 2026-02-05 16:12:06.507Z | 266.728° W |
| 10 mins | 2026-02-06 01:05:06.507Z | 116.488° SE | 2026-02-06 01:09:06.507Z | 83.946° E | 19.455° | 2026-02-06 01:15:06.507Z | 36.692° NE |
| 14 mins | 2026-02-06 02:57:06.507Z | 194.714° SSW | 2026-02-06 03:03:06.507Z | 250.869° W | 43.853° | 2026-02-06 03:11:06.507Z | 3.885° NNE |
| 5 mins | 2026-02-06 04:58:06.507Z | 284.592° WNW | 2026-02-06 05:00:06.507Z | 300.115° NW | 13.611° | 2026-02-06 05:03:06.507Z | 322.779° NNW |
| 14 mins | 2026-02-06 12:58:06.507Z | 7.694° NNE | 2026-02-06 13:05:06.507Z | 79.783° E | 35.05° | 2026-02-06 13:12:06.507Z | 144.075° SSE |
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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