COSMOS 1694, 16142
Orbit data source: Space-Track
COSMOS 1694, 16142 is a payload satellite owned by GUKOS (CIS) in LEO that was launched on Wed, 09 Oct 1985 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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16142 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
NPO PM
Mission
Spacecraft
Bus & Motor
STRELA-3, Unknown motor
Mass
225 kg wet, 225 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 COSMOS 1694
1 16142U 85094E 25298.29058183 .00000017 00000-0 32779-4 0 9992
2 16142 82.6107 51.9004 0010548 238.9277 149.1703 12.63683598846997Epoch: 2025-10-25T06:58Z
TLE epoch observation values (Epoch: 2025-10-25T06:58:26.270Z)
Latitude
27.94421°
Longitude
-82.70708°
Altitude
1,418.13 km
Speed
7.151 km/s
True Right ascension
03h 43m 18s
True Declination
27° 48' 51"
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
15:56:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,413.304 km
Perigee altitude
1,396.885 km
Semi-major axis
7,783.232 km
Eccentricity
0.00105
Inclination
82.6107°
RAAN
51.9004°
Arg. of periapsis
238.9277°
True anomaly
149.23217°
Mean anomaly
149.1703°
Eccentric anomaly
149.20124°
Mean motion
3.16085 °/min
Orbital period
113.89 mins
BSTAR
0.000032779
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Other satellites on launch #94 in the year 1985 (1985-10-09 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 1694 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. |
|---|---|---|---|---|---|---|---|
| 14 mins | 2025-10-25 20:45:05.876Z | 333.906° NNW | 2025-10-25 20:52:05.876Z | 272.467° WNW | 29.518° | 2025-10-25 20:59:05.876Z | 214.149° SW |
| 14 mins | 2025-10-26 07:38:05.876Z | 154.479° SSE | 2025-10-26 07:44:05.876Z | 92.871° ESE | 36.533° | 2025-10-26 07:52:05.876Z | 18.773° NNE |
| 13 mins | 2025-10-26 09:33:05.876Z | 229.285° WSW | 2025-10-26 09:39:05.876Z | 284.734° WNW | 29.967° | 2025-10-26 09:46:05.876Z | 348.966° N |
| 9 mins | 2025-10-26 17:40:05.876Z | 31.91° NE | 2025-10-26 17:44:05.876Z | 64.524° ENE | 17.543° | 2025-10-26 17:49:05.876Z | 103.156° ESE |
| 15 mins | 2025-10-26 19:33:05.876Z | 351.786° N | 2025-10-26 19:40:05.876Z | 233.195° WSW | 44.962° | 2025-10-26 19:48:05.876Z | 176.251° S |
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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