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: 12 hours ago
TLE from 12 hours ago
0 GONETS D1 9
1 27060U 01058F 25342.39444460 .00000030 00000-0 10975-3 0 9997
2 27060 82.5397 318.5686 0008967 25.7714 334.3823 12.63057662103743Epoch: 2025-12-08T09:28Z
TLE epoch observation values (Epoch: 2025-12-08T09:28:00.013Z)
Latitude
0.00003°
Longitude
99.17444°
Altitude
1,406.782 km
Speed
7.16 km/s
True Right ascension
21h 14m 16s
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
20:02:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,414.652 km
Perigee altitude
1,400.689 km
Semi-major axis
7,785.807 km
Eccentricity
0.0009
Inclination
82.5397°
RAAN
318.5686°
Arg. of periapsis
25.7714°
True anomaly
334.33783°
Mean anomaly
334.3823°
Eccentric anomaly
334.36007°
Mean motion
3.15928 °/min
Orbital period
113.95 mins
BSTAR
0.00010975
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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. |
|---|---|---|---|---|---|---|---|
| 16 mins | 2025-12-08 22:51:00.323Z | 169.88° S | 2025-12-08 22:59:00.323Z | 93.831° ESE | 41.591° | 2025-12-08 23:07:00.323Z | 14.427° NNE |
| 12 mins | 2025-12-09 00:49:00.323Z | 242.618° WSW | 2025-12-09 00:55:00.323Z | 296.519° NW | 24.156° | 2025-12-09 01:01:00.323Z | 345.019° N |
| 12 mins | 2025-12-09 08:54:00.323Z | 20.583° NNE | 2025-12-09 09:00:00.323Z | 72.596° E | 22.691° | 2025-12-09 09:06:00.323Z | 119.477° SE |
| 15 mins | 2025-12-09 10:48:00.323Z | 345.916° N | 2025-12-09 10:55:00.323Z | 272.998° WNW | 42.778° | 2025-12-09 11:03:00.323Z | 187.327° SSW |
| 8 mins | 2025-12-09 21:43:00.323Z | 124.239° SE | 2025-12-09 21:48:00.323Z | 82.172° E | 21.889° | 2025-12-09 21:51:00.323Z | 53.49° 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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