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: 10 hours ago
TLE from 10 hours ago
0 GONETS D1 9
1 27060U 01058F 26276.81643946 .00000016 00000-0 27416-4 0 9994
2 27060 82.5377 126.2952 0009182 61.7890 298.4128 12.63065335141540Epoch: 2026-10-03T19:35Z
TLE epoch observation values (Epoch: 2026-10-03T19:35:40.369Z)
Latitude
0.00003°
Longitude
179.85839°
Altitude
1,409.649 km
Speed
7.157 km/s
True Right ascension
08h 25m 10s
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
23:31:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,414.788 km
Perigee altitude
1,400.49 km
Semi-major axis
7,785.776 km
Eccentricity
0.00092
Inclination
82.5377°
RAAN
126.2952°
Arg. of periapsis
61.789°
True anomaly
298.32021°
Mean anomaly
298.4128°
Eccentric anomaly
298.36651°
Mean motion
3.1593 °/min
Orbital period
113.95 mins
BSTAR
0.000027416
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-10-04 12:51:44.339Z | 103.901° ESE | 2026-10-04 12:55:44.339Z | 73.935° E | 14.45° | 2026-10-04 12:58:44.339Z | 51.473° ENE |
| 15 mins | 2026-10-04 14:41:44.339Z | 181.344° SSW | 2026-10-04 14:48:44.339Z | 127.641° SE | 82.059° | 2026-10-04 14:56:44.339Z | 9.373° NNE |
| 9 mins | 2026-10-04 16:40:44.339Z | 260.72° W | 2026-10-04 16:44:44.339Z | 293.542° NW | 19.573° | 2026-10-04 16:49:44.339Z | 333.985° NNW |
| 13 mins | 2026-10-05 00:43:44.339Z | 14.434° NNE | 2026-10-05 00:49:44.339Z | 69.657° E | 33.553° | 2026-10-05 00:56:44.339Z | 131.689° SE |
| 14 mins | 2026-10-05 02:38:44.339Z | 337.909° N | 2026-10-05 02:44:44.339Z | 276.935° WNW | 50.019° | 2026-10-05 02:52:44.339Z | 199.206° 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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