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: 8 hours ago
TLE from 8 hours ago
0 GONETS D1 9
1 27060U 01058F 25307.77860830 .00000035 00000-0 13528-3 0 9995
2 27060 82.5415 340.8079 0009621 97.4732 262.7453 12.63056441 99372Epoch: 2025-11-03T18:41Z
TLE epoch observation values (Epoch: 2025-11-03T18:41:11.757Z)
Latitude
0.00001°
Longitude
17.23382°
Altitude
1,414.038 km
Speed
7.153 km/s
True Right ascension
22h 43m 13s
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
22:42:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,415.166 km
Perigee altitude
1,400.185 km
Semi-major axis
7,785.812 km
Eccentricity
0.00096
Inclination
82.5415°
RAAN
340.8079°
Arg. of periapsis
97.4732°
True anomaly
262.63595°
Mean anomaly
262.7453°
Eccentric anomaly
262.69062°
Mean motion
3.15927 °/min
Orbital period
113.95 mins
BSTAR
0.00013528
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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 | 2025-11-04 04:18:30.901Z | 228.691° WSW | 2025-11-04 04:25:30.901Z | 292.564° NW | 28.98° | 2025-11-04 04:32:30.901Z | 350.846° N |
| 10 mins | 2025-11-04 12:25:30.901Z | 27.416° NE | 2025-11-04 12:30:30.901Z | 68.407° E | 18.3° | 2025-11-04 12:35:30.901Z | 106.667° ESE |
| 14 mins | 2025-11-04 14:19:30.901Z | 350.493° N | 2025-11-04 14:26:30.901Z | 212.513° SW | 44.557° | 2025-11-04 14:33:30.901Z | 178.274° S |
| 6 mins | 2025-11-04 16:17:30.901Z | 300.013° NW | 2025-11-04 16:19:30.901Z | 284.365° WNW | 14.133° | 2025-11-04 16:23:30.901Z | 254.603° W |
| 8 mins | 2025-11-05 01:15:30.901Z | 109.082° ESE | 2025-11-05 01:19:30.901Z | 76.544° E | 17.331° | 2025-11-05 01:23:30.901Z | 45.122° ENE |
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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