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: 1 day ago
TLE from 1 day ago
0 GONETS D1 1
1 23787U 96009A 25260.10004781 .00000025 00000-0 77033-4 0 9998
2 23787 82.5732 113.7887 0010547 306.9465 223.5260 12.64098215364800Epoch: 2025-09-17T02:24Z
TLE epoch observation values (Epoch: 2025-09-17T02:24:04.13Z)
Latitude
9.47514°
Longitude
-99.7498°
Altitude
1,414.039 km
Speed
7.151 km/s
True Right ascension
19h 30m 11s
True Declination
9° 25' 27"
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
18:46:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,411.6 km
Perigee altitude
1,395.186 km
Semi-major axis
7,781.53 km
Eccentricity
0.00105
Inclination
82.5732°
RAAN
113.7887°
Arg. of periapsis
306.9465°
True anomaly
223.44285°
Mean anomaly
223.526°
Eccentric anomaly
223.48441°
Mean motion
3.16188 °/min
Orbital period
113.86 mins
BSTAR
0.000077033
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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. |
|---|---|---|---|---|---|---|---|
| 15 mins | 2025-09-18 02:48:21.499Z | 343.025° N | 2025-09-18 02:56:21.499Z | 263.112° W | 39.11° | 2025-09-18 03:03:21.499Z | 197.089° SSW |
| 11 mins | 2025-09-18 13:43:21.499Z | 130.565° SE | 2025-09-18 13:48:21.499Z | 82.994° E | 26.492° | 2025-09-18 13:54:21.499Z | 31.122° NE |
| 14 mins | 2025-09-18 15:36:21.499Z | 210.3° SW | 2025-09-18 15:42:21.499Z | 275.211° WNW | 39.239° | 2025-09-18 15:50:21.499Z | 358.549° N |
| 15 mins | 2025-09-19 01:36:21.499Z | 1.183° NNE | 2025-09-19 01:43:21.499Z | 78.763° E | 41.314° | 2025-09-19 01:51:21.499Z | 158.406° 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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