COSMOS 2330, 23792
Orbit data source: Space-Track
COSMOS 2330, 23792 is a payload satellite owned by VKS (CIS) in LEO that was launched on Mon, 19 Feb 1996 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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23792 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
NPO PM
Mission
Non-operational 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 + 1 Ant, 3.5 m
Radar Cross Section
1.583 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 COSMOS 2330
1 23792U 96009F 26266.04586068 .00000040 00000-0 16700-3 0 9997
2 23792 82.5763 281.6412 0010862 212.0368 148.0064 12.60979533407974Epoch: 2026-09-23T01:06Z
TLE epoch observation values (Epoch: 2026-09-23T01:06:02.362Z)
Latitude
0.00005°
Longitude
-96.77125°
Altitude
1,428.818 km
Speed
7.143 km/s
True Right ascension
18h 46m 33s
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
06:07:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,424.693 km
Perigee altitude
1,407.76 km
Semi-major axis
7,794.364 km
Eccentricity
0.00109
Inclination
82.5763°
RAAN
281.6412°
Arg. of periapsis
212.0368°
True anomaly
148.07227°
Mean anomaly
148.0064°
Eccentric anomaly
148.03934°
Mean motion
3.15408 °/min
Orbital period
114.14 mins
BSTAR
0.000167
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Other satellites on launch #9 in the year 1996 (1996-02-19 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 2330 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 | 2026-09-23 13:07:33.788Z | 351.148° N | 2026-09-23 13:15:33.788Z | 319.244° NNW | 81.499° | 2026-09-23 13:23:33.788Z | 177.621° S |
| 7 mins | 2026-09-23 15:06:33.788Z | 307.601° NW | 2026-09-23 15:09:33.788Z | 284.803° WNW | 15.077° | 2026-09-23 15:13:33.788Z | 254.82° W |
| 8 mins | 2026-09-24 00:06:33.788Z | 107.707° ESE | 2026-09-24 00:10:33.788Z | 74.941° E | 18.575° | 2026-09-24 00:14:33.788Z | 44.095° NE |
| 15 mins | 2026-09-24 01:57:33.788Z | 189.652° SSW | 2026-09-24 02:04:33.788Z | 323.177° NNW | 80.342° | 2026-09-24 02:12:33.788Z | 6.328° NNE |
| 7 mins | 2026-09-24 03:57:33.788Z | 273.98° WNW | 2026-09-24 04:00:33.788Z | 297.564° NW | 16.204° | 2026-09-24 04:04:33.788Z | 328.199° NNW |
| 14 mins | 2026-09-24 11:59:33.788Z | 9.283° NNE | 2026-09-24 12:06:33.788Z | 78.488° E | 40.795° | 2026-09-24 12:13:33.788Z | 140.555° 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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