GONETS D1 1, 23787
Orbit data source: Space-Track
GONETS D1 1, 23787 is a payload satellite owned by Gonets (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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23787 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
NPO PM
Mission
Non-operational Civil 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
1.798 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 GONETS D1 1
1 23787U 96009A 25360.11065705 .00000014 00000-0 15184-4 0 9990
2 23787 82.5764 49.7321 0012241 78.4433 309.1261 12.64102201377442Epoch: 2025-12-26T02:39Z
TLE epoch observation values (Epoch: 2025-12-26T02:39:20.769Z)
Latitude
27.24721°
Longitude
-81.13216°
Altitude
1,403.244 km
Speed
7.164 km/s
True Right ascension
03h 34m 14s
True Declination
27° 07' 09"
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
14:47:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,412.902 km
Perigee altitude
1,393.851 km
Semi-major axis
7,781.513 km
Eccentricity
0.00122
Inclination
82.5764°
RAAN
49.7321°
Arg. of periapsis
78.4433°
True anomaly
309.01718°
Mean anomaly
309.1261°
Eccentric anomaly
309.07165°
Mean motion
3.16189 °/min
Orbital period
113.86 mins
BSTAR
0.000015184
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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.GONETS D1 1 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 | 2025-12-26 16:25:31.760Z | 336.356° NNW | 2025-12-26 16:32:31.760Z | 276.046° WNW | 31.616° | 2025-12-26 16:39:31.760Z | 211.75° SW |
| 13 mins | 2025-12-27 03:18:31.760Z | 151.175° SSE | 2025-12-27 03:24:31.760Z | 94.793° ESE | 34.091° | 2025-12-27 03:31:31.760Z | 23.725° NE |
| 13 mins | 2025-12-27 05:13:31.760Z | 225.184° WSW | 2025-12-27 05:19:31.760Z | 282.891° WNW | 31.968° | 2025-12-27 05:26:31.760Z | 350.397° N |
| 8 mins | 2025-12-27 13:20:31.760Z | 34.117° NE | 2025-12-27 13:24:31.760Z | 65.926° ENE | 15.625° | 2025-12-27 13:28:31.760Z | 96.172° ESE |
| 13 mins | 2025-12-27 15:13:31.760Z | 354.136° N | 2025-12-27 15:20:31.760Z | 128.989° SE | 44.769° | 2025-12-27 15:26:31.760Z | 171.333° 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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