GONETS D1 6, 24730
Orbit data source: Space-Track
GONETS D1 6, 24730 is a payload satellite owned by Gonets (CIS) in LEO that was launched on Fri, 14 Feb 1997 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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24730 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 6
1 24730U 97006F 25259.94282267 .00000047 00000-0 20315-3 0 9996
2 24730 82.6032 70.8127 0002227 194.1330 165.9700 12.62488998317194Epoch: 2025-09-16T22:37Z
TLE epoch observation values (Epoch: 2025-09-16T22:37:39.878Z)
Latitude
0.00004°
Longitude
95.27067°
Altitude
1,417.102 km
Speed
7.151 km/s
True Right ascension
04h 43m 15s
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
16:49:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,411.742 km
Perigee altitude
1,408.273 km
Semi-major axis
7,788.144 km
Eccentricity
0.00022
Inclination
82.6032°
RAAN
70.8127°
Arg. of periapsis
194.133°
True anomaly
165.97619°
Mean anomaly
165.97°
Eccentric anomaly
165.97309°
Mean motion
3.15785 °/min
Orbital period
114 mins
BSTAR
0.00020315
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Other satellites on launch #6 in the year 1997 (1997-02-14 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 6 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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2025-09-18 00:01:20.935Z | 331.017° NNW | 2025-09-18 00:05:20.935Z | 275.326° WNW | 38.872° | 2025-09-18 00:13:20.935Z | 196.493° SSW |
| 12 mins | 2025-09-18 10:53:20.935Z | 133.489° SE | 2025-09-18 10:58:20.935Z | 87.618° E | 27.153° | 2025-09-18 11:05:20.935Z | 27.936° NE |
| 14 mins | 2025-09-18 12:46:20.935Z | 210.001° SW | 2025-09-18 12:53:20.935Z | 287.296° WNW | 38.748° | 2025-09-18 13:00:20.935Z | 356.653° N |
| 15 mins | 2025-09-18 22:47:20.935Z | 359.949° N | 2025-09-18 22:54:20.935Z | 70.107° E | 41.817° | 2025-09-18 23:02:20.935Z | 159.492° 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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