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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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: 6 hours ago
TLE from 6 hours ago
0 GONETS D1 9
1 27060U 01058F 26068.96389341 .00000024 00000-0 74997-4 0 9990
2 27060 82.5352 259.7503 0008537 166.0144 194.1186 12.63060790115302Epoch: 2026-03-09T23:08Z
TLE epoch observation values (Epoch: 2026-03-09T23:08:00.390Z)
Latitude
0.00003°
Longitude
105.09939°
Altitude
1,419.516 km
Speed
7.148 km/s
True Right ascension
17h 19m 00s
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
09:32:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,414.304 km
Perigee altitude
1,401.011 km
Semi-major axis
7,785.795 km
Eccentricity
0.00085
Inclination
82.5352°
RAAN
259.7503°
Arg. of periapsis
166.0144°
True anomaly
194.09476°
Mean anomaly
194.1186°
Eccentric anomaly
194.10668°
Mean motion
3.15928 °/min
Orbital period
113.95 mins
BSTAR
0.000074997
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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 | 2026-03-10 12:31:42.791Z | 155.514° SSE | 2026-03-10 12:38:42.791Z | 95.305° ESE | 34.898° | 2026-03-10 12:46:42.791Z | 20.363° NNE |
| 13 mins | 2026-03-10 14:27:42.791Z | 225.946° WSW | 2026-03-10 14:33:42.791Z | 281.341° WNW | 31.401° | 2026-03-10 14:40:42.791Z | 349.338° N |
| 8 mins | 2026-03-10 22:35:42.791Z | 36.792° NE | 2026-03-10 22:38:42.791Z | 61.118° ENE | 16.436° | 2026-03-10 22:43:42.791Z | 99.616° ESE |
| 14 mins | 2026-03-11 00:28:42.791Z | 353.199° N | 2026-03-11 00:34:42.791Z | 10.002° NNE | 44.815° | 2026-03-11 00:42:42.791Z | 173.706° S |
| 7 mins | 2026-03-11 02:25:42.791Z | 306.985° NW | 2026-03-11 02:28:42.791Z | 282.895° WNW | 16.13° | 2026-03-11 02:32:42.791Z | 251.621° W |
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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