COSMOS 2214, 22185
Orbit data source: Space-Track
COSMOS 2214, 22185 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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22185 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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 COSMOS 2214
1 22185U 92068D 25256.24026169 .00000029 00000-0 10200-3 0 9990
2 22185 82.5962 169.9483 0009855 60.1250 108.3018 12.61593792514728Epoch: 2025-09-13T05:45Z
TLE epoch observation values (Epoch: 2025-09-13T05:45:58.61Z)
Latitude
11.32544°
Longitude
-90.50633°
Altitude
1,420.772 km
Speed
7.15 km/s
True Right ascension
23h 13m 51s
True Declination
11° 15' 54"
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
16:04:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,421.373 km
Perigee altitude
1,406.015 km
Semi-major axis
7,791.831 km
Eccentricity
0.00099
Inclination
82.5962°
RAAN
169.9483°
Arg. of periapsis
60.125°
True anomaly
108.40898°
Mean anomaly
108.3018°
Eccentric anomaly
108.35539°
Mean motion
3.15561 °/min
Orbital period
114.08 mins
BSTAR
0.000102
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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 2214 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 | 2025-09-14 04:20:13.200Z | 24.874° NE | 2025-09-14 04:25:13.200Z | 63.705° ENE | 17.616° | 2025-09-14 04:30:13.200Z | 102.566° ESE |
| 15 mins | 2025-09-14 06:14:13.200Z | 351.699° N | 2025-09-14 06:21:13.200Z | 315.333° NNW | 44.918° | 2025-09-14 06:29:13.200Z | 176.368° S |
| 7 mins | 2025-09-14 08:12:13.200Z | 306.086° NW | 2025-09-14 08:15:13.200Z | 282.634° WNW | 15.088° | 2025-09-14 08:19:13.200Z | 252.601° W |
| 8 mins | 2025-09-14 17:12:13.200Z | 104.421° ESE | 2025-09-14 17:15:13.200Z | 80.127° E | 16.786° | 2025-09-14 17:20:13.200Z | 41.88° NE |
| 15 mins | 2025-09-14 19:02:13.200Z | 187.819° SSW | 2025-09-14 19:09:13.200Z | 250.834° W | 44.897° | 2025-09-14 19:17:13.200Z | 6.637° NNE |
| 8 mins | 2025-09-14 21:02:13.200Z | 270.068° WNW | 2025-09-14 21:05:13.200Z | 293.623° NW | 15.814° | 2025-09-14 21:10:13.200Z | 332.151° NNW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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