GONETS D1 7, 27058
Orbit data source: Space-Track
GONETS D1 7, 27058 is a payload satellite owned by Gonets (CIS) in LEO that was launched on Fri, 28 Dec 2001 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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27058 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: 11 hours ago
TLE from 11 hours ago
0 GONETS D1 7
1 27058U 01058D 25292.22975753 .00000023 00000-0 71100-4 0 9994
2 27058 82.5393 356.4370 0003440 163.3175 196.8029 12.62079539 96597Epoch: 2025-10-19T05:30Z
TLE epoch observation values (Epoch: 2025-10-19T05:30:51.050Z)
Latitude
-0.00009°
Longitude
-114.22513°
Altitude
1,419.668 km
Speed
7.15 km/s
True Right ascension
23h 45m 44s
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
11:32:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,414.375 km
Perigee altitude
1,409.016 km
Semi-major axis
7,789.832 km
Eccentricity
0.00034
Inclination
82.5393°
RAAN
356.437°
Arg. of periapsis
163.3175°
True anomaly
196.79151°
Mean anomaly
196.8029°
Eccentric anomaly
196.7972°
Mean motion
3.15683 °/min
Orbital period
114.04 mins
BSTAR
0.0000711
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Other satellites on launch #58 in the year 2001 (2001-12-28 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 7 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. |
|---|---|---|---|---|---|---|---|
| 13 mins | 2025-10-19 17:33:24.418Z | 332.027° NNW | 2025-10-19 17:40:24.418Z | 271.19° WNW | 27.617° | 2025-10-19 17:46:24.418Z | 220.335° SW |
| 14 mins | 2025-10-20 04:26:24.418Z | 160.549° S | 2025-10-20 04:33:24.418Z | 88.092° E | 38.423° | 2025-10-20 04:40:24.418Z | 19.101° NNE |
| 13 mins | 2025-10-20 06:22:24.418Z | 232.764° WSW | 2025-10-20 06:28:24.418Z | 286.064° WNW | 28.01° | 2025-10-20 06:35:24.418Z | 347.987° N |
| 10 mins | 2025-10-20 14:29:24.418Z | 27.321° NE | 2025-10-20 14:34:24.418Z | 69.363° E | 19.46° | 2025-10-20 14:39:24.418Z | 108.45° ESE |
| 14 mins | 2025-10-20 16:23:24.418Z | 349.042° N | 2025-10-20 16:30:24.418Z | 228.173° WSW | 44.242° | 2025-10-20 16:37:24.418Z | 180.787° SSW |
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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