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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 GONETS D1 6
1 24730U 97006F 26308.06105737 .00000017 00000-0 32981-4 0 9991
2 24730 82.6083 168.1593 0002946 14.4401 345.6774 12.62501822369321Epoch: 2026-11-04T01:27Z
TLE epoch observation values (Epoch: 2026-11-04T01:27:55.356Z)
Latitude
-0.00003°
Longitude
102.86386°
Altitude
1,413.142 km
Speed
7.155 km/s
True Right ascension
11h 12m 38s
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
11:11:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,412.249 km
Perigee altitude
1,407.66 km
Semi-major axis
7,788.091 km
Eccentricity
0.00029
Inclination
82.6083°
RAAN
168.1593°
Arg. of periapsis
14.4401°
True anomaly
345.66905°
Mean anomaly
345.6774°
Eccentric anomaly
345.67322°
Mean motion
3.15789 °/min
Orbital period
114 mins
BSTAR
0.000032981
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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. |
|---|---|---|---|---|---|---|---|
| 14 mins | 2026-11-04 16:47:25.542Z | 227.852° WSW | 2026-11-04 16:54:25.542Z | 287.075° WNW | 32.954° | 2026-11-04 17:01:25.542Z | 348.621° N |
| 10 mins | 2026-11-05 00:55:25.542Z | 29.151° NE | 2026-11-05 00:59:25.542Z | 61.826° ENE | 20.032° | 2026-11-05 01:05:25.542Z | 108.713° ESE |
| 15 mins | 2026-11-05 02:48:25.542Z | 350.302° N | 2026-11-05 02:55:25.542Z | 298.933° NW | 80.557° | 2026-11-05 03:03:25.542Z | 179.295° S |
| 6 mins | 2026-11-05 04:46:25.542Z | 305.662° NW | 2026-11-05 04:49:25.542Z | 282.937° WNW | 14.295° | 2026-11-05 04:52:25.542Z | 260.439° W |
| 9 mins | 2026-11-05 13:45:25.542Z | 109.373° ESE | 2026-11-05 13:49:25.542Z | 76.149° E | 19.08° | 2026-11-05 13:54:25.542Z | 38.576° NE |
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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