NEOSSAT, 39089
Orbit data source: Space-Track
NEOSSAT, 39089 is a payload satellite owned by CSA (CA) in SSO that was launched on Mon, 25 Feb 2013 UTC via a PSLV launch vehicle from the Sirharikota (SRI). 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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39089 intel report (Beta)
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Identifier
Orbit
Country
CARelated business
Manufacturer
MSCI
Mission
Operational Civil Ast/Early Warn
Bus & Motor
MOST?, Unknown motor
Mass
74 kg wet, 74 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 0.9 m
Radar Cross Section
2.340 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 22 hours ago
TLE from 22 hours ago
0 NEOSSAT
1 39089U 13009D 26094.48057680 .00000288 00000-0 11425-3 0 9995
2 39089 98.4160 276.2696 0012168 105.0144 255.2390 14.35799961686167Epoch: 2026-04-04T11:32Z
TLE epoch observation values (Epoch: 2026-04-04T11:32:01.835Z)
Latitude
0°
Longitude
-89.53779°
Altitude
777.582 km
Speed
7.464 km/s
True Right ascension
18h 25m 04s
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
15:00:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
778.23 km
Perigee altitude
760.835 km
Semi-major axis
7,147.67 km
Eccentricity
0.00122
Inclination
98.416°
RAAN
276.2696°
Arg. of periapsis
105.0144°
True anomaly
255.10422°
Mean anomaly
255.239°
Eccentric anomaly
255.1716°
Mean motion
3.59167 °/min
Orbital period
100.23 mins
BSTAR
0.00011425
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Other satellites on launch #9 in the year 2013 (2013-02-25 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.NEOSSAT 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 | 2026-04-05 11:05:20.695Z | 119.782° SE | 2026-04-05 11:09:20.695Z | 62.622° ENE | 23.999° | 2026-04-05 11:12:20.695Z | 18.506° NNE |
| 7 mins | 2026-04-05 12:45:20.695Z | 210.686° SW | 2026-04-05 12:48:20.695Z | 268.909° W | 29.743° | 2026-04-05 12:52:20.695Z | 326.371° NNW |
| 8 mins | 2026-04-06 00:55:20.695Z | 16.421° NNE | 2026-04-06 00:58:20.695Z | 53.194° ENE | 44.466° | 2026-04-06 01:03:20.695Z | 191.517° 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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