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: 15 hours ago
TLE from 15 hours ago
0 GONETS D1 9
1 27060U 01058F 25260.80552521 .00000007 00000-0 -19997-4 0 9999
2 27060 82.5457 10.9627 0008288 196.6082 163.4739 12.63054727 93441Epoch: 2025-09-17T19:19Z
TLE epoch observation values (Epoch: 2025-09-17T19:19:57.378Z)
Latitude
-0.00002°
Longitude
83.99742°
Altitude
1,419.281 km
Speed
7.148 km/s
True Right ascension
00h 43m 51s
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
03:22:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,414.135 km
Perigee altitude
1,401.229 km
Semi-major axis
7,785.819 km
Eccentricity
0.00083
Inclination
82.5457°
RAAN
10.9627°
Arg. of periapsis
196.6082°
True anomaly
163.50089°
Mean anomaly
163.4739°
Eccentric anomaly
163.4874°
Mean motion
3.15927 °/min
Orbital period
113.95 mins
BSTAR
-0.000019997
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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. |
|---|---|---|---|---|---|---|---|
| 15 mins | 2025-09-18 18:45:22.696Z | 1.159° NNE | 2025-09-18 18:52:22.696Z | 68.97° E | 40.483° | 2025-09-18 19:00:22.696Z | 156.184° SSE |
| 11 mins | 2025-09-18 20:42:22.696Z | 320.376° NNW | 2025-09-18 20:47:22.696Z | 273.143° WNW | 24.852° | 2025-09-18 20:53:22.696Z | 224.614° SW |
| 14 mins | 2025-09-19 07:33:22.696Z | 164.365° S | 2025-09-19 07:39:22.696Z | 104.961° ESE | 40.384° | 2025-09-19 07:47:22.696Z | 16.104° NNE |
| 12 mins | 2025-09-19 09:29:22.696Z | 238.779° WSW | 2025-09-19 09:35:22.696Z | 292.1° WNW | 25.63° | 2025-09-19 09:41:22.696Z | 343.803° 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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