SERVIS 2, 36588
Orbit data source: Space-Track
SERVIS 2, 36588 is a payload satellite owned by USEF (JP) in SSO that was launched on Wed, 02 Jun 2010 UTC via an ROKOT 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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36588 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
JP / JPNRelated business
Manufacturer
MELCO
Mission
Commercial Technology
Bus & Motor
SERVIS, Unknown motor
Mass
740 kg wet, ~700 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 5.1 m
Radar Cross Section
8.092 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 SERVIS 2
1 36588U 10023A 26016.94864677 -.00000001 00000-0 11381-3 0 9991
2 36588 100.4241 206.8481 0016947 259.0888 237.2712 13.16042744750873Epoch: 2026-01-16T22:46Z
TLE epoch observation values (Epoch: 2026-01-16T22:46:03.080Z)
Latitude
42.99053°
Longitude
-61.22085°
Altitude
1,213.024 km
Speed
7.248 km/s
True Right ascension
02h 26m 41s
True Declination
42° 49' 46"
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
09:41:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,210.096 km
Perigee altitude
1,184.42 km
Semi-major axis
7,575.395 km
Eccentricity
0.00169
Inclination
100.4241°
RAAN
206.8481°
Arg. of periapsis
259.0888°
True anomaly
237.10802°
Mean anomaly
237.2712°
Eccentric anomaly
237.18959°
Mean motion
3.29181 °/min
Orbital period
109.36 mins
BSTAR
0.00011381
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Other satellites on launch #23 in the year 2010 (2010-06-02 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.SERVIS 2 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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2026-01-17 10:59:48.012Z | 110.697° ESE | 2026-01-17 11:04:48.012Z | 64.097° ENE | 24.028° | 2026-01-17 11:10:48.012Z | 6.861° NNE |
| 12 mins | 2026-01-17 12:46:48.012Z | 180.405° SSW | 2026-01-17 12:52:48.012Z | 275.512° WNW | 41.086° | 2026-01-17 12:58:48.012Z | 336.343° NNW |
| 10 mins | 2026-01-18 00:15:48.012Z | 46.879° ENE | 2026-01-18 00:20:48.012Z | 99.452° ESE | 23.965° | 2026-01-18 00:25:48.012Z | 147.103° SSE |
| 12 mins | 2026-01-18 02:02:48.012Z | 4.688° NNE | 2026-01-18 02:08:48.012Z | 280.805° WNW | 39.916° | 2026-01-18 02:14:48.012Z | 217.001° SW |
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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