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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 GONETS D1 9
1 27060U 01058F 26307.47142830 .00000045 00000-0 18829-3 0 9996
2 27060 82.5362 106.6004 0008147 356.3617 3.7414 12.63066519145414Epoch: 2026-11-03T11:18Z
TLE epoch observation values (Epoch: 2026-11-03T11:18:51.405Z)
Latitude
0.00001°
Longitude
-105.8474°
Altitude
1,406.71 km
Speed
7.16 km/s
True Right ascension
07h 06m 24s
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
18:55:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,413.977 km
Perigee altitude
1,401.291 km
Semi-major axis
7,785.771 km
Eccentricity
0.00081
Inclination
82.5362°
RAAN
106.6004°
Arg. of periapsis
356.3617°
True anomaly
3.7475°
Mean anomaly
3.7414°
Eccentric anomaly
3.74445°
Mean motion
3.1593 °/min
Orbital period
113.95 mins
BSTAR
0.00018829
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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 | 2026-11-03 23:20:27.643Z | 341.042° N | 2026-11-03 23:27:27.643Z | 273.594° WNW | 52.456° | 2026-11-03 23:35:27.643Z | 197.334° SSW |
| 12 mins | 2026-11-04 10:14:27.643Z | 137.176° SSE | 2026-11-04 10:20:27.643Z | 82.424° E | 31.404° | 2026-11-04 10:26:27.643Z | 30.204° NE |
| 14 mins | 2026-11-04 12:08:27.643Z | 212.185° SW | 2026-11-04 12:14:27.643Z | 274.593° WNW | 52.19° | 2026-11-04 12:22:27.643Z | 357.66° N |
| 14 mins | 2026-11-04 22:09:27.643Z | 0.984° NNE | 2026-11-04 22:16:27.643Z | 95.205° ESE | 64.17° | 2026-11-04 22:23:27.643Z | 159.611° S |
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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