GONETS D1 9, 27060
Orbit data source: Space-Track
GONETS D1 9, 27060 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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27060 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: 14 hours ago
TLE from 14 hours ago
0 GONETS D1 9
1 27060U 01058F 25295.50066309 .00000039 00000-0 15600-3 0 9998
2 27060 82.5438 348.6925 0009476 122.4462 237.7547 12.63056059 97829Epoch: 2025-10-22T12:00Z
TLE epoch observation values (Epoch: 2025-10-22T12:00:57.290Z)
Latitude
-0.00005°
Longitude
137.28041°
Altitude
1,417.029 km
Speed
7.15 km/s
True Right ascension
23h 14m 46s
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
21:18:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,415.055 km
Perigee altitude
1,400.299 km
Semi-major axis
7,785.814 km
Eccentricity
0.00095
Inclination
82.5438°
RAAN
348.6925°
Arg. of periapsis
122.4462°
True anomaly
237.66292°
Mean anomaly
237.7547°
Eccentric anomaly
237.7088°
Mean motion
3.15927 °/min
Orbital period
113.95 mins
BSTAR
0.000156
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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 9 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 | 2025-10-23 03:19:06.935Z | 146.95° SSE | 2025-10-23 03:26:06.935Z | 86.418° E | 30.469° | 2025-10-23 03:33:06.935Z | 25.166° NE |
| 14 mins | 2025-10-23 05:14:06.935Z | 216.453° SW | 2025-10-23 05:21:06.935Z | 289.694° WNW | 35.701° | 2025-10-23 05:28:06.935Z | 354.633° N |
| 5 mins | 2025-10-23 13:23:06.935Z | 42.342° NE | 2025-10-23 13:25:06.935Z | 57.507° ENE | 13.071° | 2025-10-23 13:28:06.935Z | 80.221° E |
| 15 mins | 2025-10-23 15:15:06.935Z | 357.589° N | 2025-10-23 15:22:06.935Z | 91.921° ESE | 43.754° | 2025-10-23 15:30:06.935Z | 165.91° S |
| 9 mins | 2025-10-23 17:12:06.935Z | 312.904° NW | 2025-10-23 17:16:06.935Z | 278.082° WNW | 20.07° | 2025-10-23 17:21:06.935Z | 238.044° WSW |
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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