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: 11 hours ago
TLE from 11 hours ago
0 GONETS D1 9
1 27060U 01058F 25312.45214634 .00000010 00000-0 -15123-5 0 9990
2 27060 82.5409 337.8059 0009600 88.0460 272.1731 12.63056533 99961Epoch: 2025-11-08T10:51Z
TLE epoch observation values (Epoch: 2025-11-08T10:51:05.443Z)
Latitude
-0.00002°
Longitude
127.15166°
Altitude
1,412.807 km
Speed
7.154 km/s
True Right ascension
22h 31m 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
18:29:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,415.149 km
Perigee altitude
1,400.201 km
Semi-major axis
7,785.812 km
Eccentricity
0.00096
Inclination
82.5409°
RAAN
337.8059°
Arg. of periapsis
88.046°
True anomaly
272.06317°
Mean anomaly
272.1731°
Eccentric anomaly
272.11813°
Mean motion
3.15927 °/min
Orbital period
113.95 mins
BSTAR
-0.0000015123
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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 | 2025-11-09 02:08:46.783Z | 170.525° S | 2025-11-09 02:15:46.783Z | 109.247° ESE | 41.953° | 2025-11-09 02:23:46.783Z | 14.306° NNE |
| 11 mins | 2025-11-09 04:06:46.783Z | 247.137° WSW | 2025-11-09 04:11:46.783Z | 291.85° WNW | 23.491° | 2025-11-09 04:17:46.783Z | 342.378° N |
| 11 mins | 2025-11-09 12:11:46.783Z | 23.635° NE | 2025-11-09 12:16:46.783Z | 68.547° E | 23.439° | 2025-11-09 12:22:46.783Z | 118.64° SE |
| 14 mins | 2025-11-09 14:05:46.783Z | 344.149° N | 2025-11-09 14:12:46.783Z | 249.363° W | 41.962° | 2025-11-09 14:19:46.783Z | 189.304° 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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