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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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: 14 hours ago
TLE from 14 hours ago
0 GONETS D1 6
1 24730U 97006F 26127.93159046 .00000039 00000-0 15949-3 0 9996
2 24730 82.6047 282.6692 0003248 60.7645 299.3771 12.62498345346594Epoch: 2026-05-07T22:21Z
TLE epoch observation values (Epoch: 2026-05-07T22:21:29.415Z)
Latitude
-0.00001°
Longitude
81.52599°
Altitude
1,414.139 km
Speed
7.154 km/s
True Right ascension
18h 50m 40s
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
20:51:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,412.498 km
Perigee altitude
1,407.439 km
Semi-major axis
7,788.106 km
Eccentricity
0.00032
Inclination
82.6047°
RAAN
282.6692°
Arg. of periapsis
60.7645°
True anomaly
299.34466°
Mean anomaly
299.3771°
Eccentric anomaly
299.36088°
Mean motion
3.15788 °/min
Orbital period
114 mins
BSTAR
0.00015949
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-05-08 19:55:54.817Z | 41.826° NE | 2026-05-08 19:57:54.817Z | 56.442° ENE | 11.902° | 2026-05-08 20:00:54.817Z | 78.332° E |
| 15 mins | 2026-05-08 21:47:54.817Z | 359.112° N | 2026-05-08 21:54:54.817Z | 79.802° E | 42.854° | 2026-05-08 22:02:54.817Z | 162.553° S |
| 10 mins | 2026-05-08 23:44:54.817Z | 315.889° NNW | 2026-05-08 23:48:54.817Z | 280.712° WNW | 21.85° | 2026-05-08 23:54:54.817Z | 232.123° WSW |
| 14 mins | 2026-05-09 10:35:54.817Z | 171.342° S | 2026-05-09 10:41:54.817Z | 111.666° ESE | 42.795° | 2026-05-09 10:49:54.817Z | 13.148° NNE |
| 11 mins | 2026-05-09 12:32:54.817Z | 248.442° W | 2026-05-09 12:37:54.817Z | 291.463° WNW | 22.387° | 2026-05-09 12:43:54.817Z | 341.267° N |
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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