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: 8 hours ago
TLE from 8 hours ago
0 SERVIS 2
1 36588U 10023A 25307.80061259 -.00000002 00000-0 11194-3 0 9996
2 36588 100.4260 133.7842 0017827 68.8803 302.0993 13.16036582741127Epoch: 2025-11-03T19:12Z
TLE epoch observation values (Epoch: 2025-11-03T19:12:52.927Z)
Latitude
10.5783°
Longitude
160.30761°
Altitude
1,194.7 km
Speed
7.261 km/s
True Right ascension
08h 47m 17s
True Declination
10° 31' 12"
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
22:58:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,210.786 km
Perigee altitude
1,183.777 km
Semi-major axis
7,575.419 km
Eccentricity
0.00178
Inclination
100.426°
RAAN
133.7842°
Arg. of periapsis
68.8803°
True anomaly
301.92604°
Mean anomaly
302.0993°
Eccentric anomaly
302.01269°
Mean motion
3.2918 °/min
Orbital period
109.36 mins
BSTAR
0.00011194
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-11-04 03:04:28.144Z | 335.316° NNW | 2025-11-04 03:07:28.144Z | 303.188° NW | 21.559° | 2025-11-04 03:12:28.144Z | 255.612° W |
| 12 mins | 2025-11-04 11:42:28.144Z | 135.611° SSE | 2025-11-04 11:48:28.144Z | 53.97° ENE | 37.137° | 2025-11-04 11:54:28.144Z | 355.39° N |
| 10 mins | 2025-11-04 13:31:28.144Z | 214.138° SW | 2025-11-04 13:35:28.144Z | 257.893° W | 26.543° | 2025-11-04 13:41:28.144Z | 320.829° NNW |
| 12 mins | 2025-11-05 00:58:28.144Z | 29.539° NE | 2025-11-05 01:03:28.144Z | 89.496° E | 38.651° | 2025-11-05 01:10:28.144Z | 176.986° S |
| 10 mins | 2025-11-05 02:46:28.144Z | 349.512° N | 2025-11-05 02:51:28.144Z | 295.09° NW | 26.368° | 2025-11-05 02:56:28.144Z | 245.386° WSW |
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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