COSMOS 192, 3047
Orbit data source: Space-Track
COSMOS 192, 3047 is a payload satellite owned by OKB-10 (CIS) in LEO that was launched on Thu, 23 Nov 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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3047 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
775 kg wet, 775 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: 13 hours ago
TLE from 13 hours ago
0 COSMOS 192
1 3047U 67116A 26123.66411843 .00000303 00000-0 73085-4 0 9995
2 3047 74.0104 100.4031 0009537 276.6878 83.3200 14.57560385 92145Epoch: 2026-05-03T15:56Z
TLE epoch observation values (Epoch: 2026-05-03T15:56:19.832Z)
Latitude
-0.00008°
Longitude
-0.24398°
Altitude
702.919 km
Speed
7.505 km/s
True Right ascension
06h 41m 36s
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
12:23:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
705.414 km
Perigee altitude
691.916 km
Semi-major axis
7,076.802 km
Eccentricity
0.00095
Inclination
74.0104°
RAAN
100.4031°
Arg. of periapsis
276.6878°
True anomaly
83.42856°
Mean anomaly
83.32°
Eccentric anomaly
83.37428°
Mean motion
3.64576 °/min
Orbital period
98.74 mins
BSTAR
0.000073085
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Other satellites on launch #116 in the year 1967 (1967-11-23 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 192 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 | 2026-05-04 08:57:52.529Z | 5.62° NNE | 2026-05-04 09:01:52.529Z | 69.572° E | 26.398° | 2026-05-04 09:04:52.529Z | 117.149° SE |
| 6 mins | 2026-05-04 10:39:52.529Z | 300.804° NW | 2026-05-04 10:41:52.529Z | 265.218° W | 25.192° | 2026-05-04 10:45:52.529Z | 204.321° SW |
| 8 mins | 2026-05-04 23:21:52.529Z | 187.778° SSW | 2026-05-04 23:25:52.529Z | 71.961° E | 42.82° | 2026-05-04 23:29:52.529Z | 23.952° NE |
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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