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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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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 GONETS D1 1
1 23787U 96009A 26194.73868264 .00000020 00000-0 49686-4 0 9996
2 23787 82.5772 281.8935 0010586 348.2163 128.5288 12.64108000402667Epoch: 2026-07-13T17:43Z
TLE epoch observation values (Epoch: 2026-07-13T17:43:42.180Z)
Latitude
62.31143°
Longitude
-109.9539°
Altitude
1,421.822 km
Speed
7.153 km/s
True Right ascension
05h 50m 21s
True Declination
62° 10' 54"
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
17:35:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,411.59 km
Perigee altitude
1,395.115 km
Semi-major axis
7,781.49 km
Eccentricity
0.00106
Inclination
82.5772°
RAAN
281.8935°
Arg. of periapsis
348.2163°
True anomaly
128.62362°
Mean anomaly
128.5288°
Eccentric anomaly
128.57622°
Mean motion
3.16191 °/min
Orbital period
113.86 mins
BSTAR
0.000049686
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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 | 2026-07-14 06:29:41.006Z | 181.77° SSW | 2026-07-14 06:37:41.006Z | 43.782° NE | 44.582° | 2026-07-14 06:44:41.006Z | 9.228° NNE |
| 10 mins | 2026-07-14 08:28:41.006Z | 259.398° W | 2026-07-14 08:32:41.006Z | 291.587° WNW | 18.257° | 2026-07-14 08:38:41.006Z | 338.587° N |
| 13 mins | 2026-07-14 16:31:41.006Z | 15.353° NNE | 2026-07-14 16:37:41.006Z | 72.053° E | 28.936° | 2026-07-14 16:44:41.006Z | 132.432° SE |
| 13 mins | 2026-07-14 18:26:41.006Z | 337.078° NNW | 2026-07-14 18:32:41.006Z | 270.99° WNW | 37.577° | 2026-07-14 18:39:41.006Z | 201.015° SSW |
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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