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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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
OKB-10
Mission
Defense Navigation
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
Cyl + 1 Rod, 8.5 m
Radar Cross Section
9.978 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 COSMOS 192
1 03047U 67116A 25259.19877303 .00000316 00000-0 76271-4 0 9993
2 03047 74.0134 177.1146 0007178 45.2680 314.9067 14.57333188 58714Epoch: 2025-09-16T04:46Z
TLE epoch observation values (Epoch: 2025-09-16T04:46:13.989Z)
Latitude
-0.00007°
Longitude
110.16378°
Altitude
700.847 km
Speed
7.508 km/s
True Right ascension
11h 48m 27s
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
05:17:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
704.481 km
Perigee altitude
694.32 km
Semi-major axis
7,077.537 km
Eccentricity
0.00072
Inclination
74.0134°
RAAN
177.1146°
Arg. of periapsis
45.268°
True anomaly
314.84841°
Mean anomaly
314.9067°
Eccentric anomaly
314.87756°
Mean motion
3.64519 °/min
Orbital period
98.76 mins
BSTAR
0.000076271
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-09-16 19:42:24.571Z | 191.339° SSW | 2025-09-16 19:47:24.571Z | 81.22° E | 43.819° | 2025-09-16 19:51:24.571Z | 23.055° NE |
| 8 mins | 2025-09-17 06:03:24.571Z | 336.74° NNW | 2025-09-17 06:07:24.571Z | 202.477° SSW | 43.271° | 2025-09-17 06:11:24.571Z | 168.164° S |
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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