ALSAT 2B, 41786
Orbit data source: Space-Track
ALSAT 2B, 41786 is a payload satellite owned by ASAL (DZ) in SSO that was launched on Mon, 26 Sep 2016 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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41786 intel report (Beta)
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Identifier
Orbit
Country
DZ / ALGRelated business
Manufacturer
Airbus/Toulouse
Mission
Operational Civil Imaging
Bus & Motor
MYRIADE, AOCS
Mass
117 kg wet, 117 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 0.9 m
Radar Cross Section
0.912 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 ALSAT 2B
1 41786U 16059D 26172.49656706 .00000885 00000-0 15266-3 0 9992
2 41786 97.9891 234.6861 0001370 117.9305 242.2040 14.70878344521400Epoch: 2026-06-21T11:55Z
TLE epoch observation values (Epoch: 2026-06-21T11:55:03.393Z)
Latitude
-0.0001°
Longitude
146.22598°
Altitude
661.722 km
Speed
7.526 km/s
True Right ascension
15h 38m 44s
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
21:37:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
656.286 km
Perigee altitude
654.359 km
Semi-major axis
7,033.46 km
Eccentricity
0.00014
Inclination
97.9891°
RAAN
234.6861°
Arg. of periapsis
117.9305°
True anomaly
242.19011°
Mean anomaly
242.204°
Eccentric anomaly
242.19706°
Mean motion
3.67951 °/min
Orbital period
97.84 mins
BSTAR
0.00015266
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Other satellites on launch #59 in the year 2016 (2016-09-26 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.ALSAT 2B 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 | 2026-06-22 16:14:58.789Z | 38.139° NE | 2026-06-22 16:18:58.789Z | 101.148° ESE | 24.014° | 2026-06-22 16:21:58.789Z | 148.954° SSE |
| 6 mins | 2026-06-22 17:52:58.789Z | 337.985° N | 2026-06-22 17:55:58.789Z | 280.718° WNW | 24.469° | 2026-06-22 17:58:58.789Z | 235.984° WSW |
| 5 mins | 2026-06-23 03:15:58.789Z | 102.949° ESE | 2026-06-23 03:17:58.789Z | 66.607° ENE | 21.704° | 2026-06-23 03:20:58.789Z | 19.64° NNE |
| 6 mins | 2026-06-23 04:51:58.789Z | 211.063° SW | 2026-06-23 04:54:58.789Z | 272.699° WNW | 27.461° | 2026-06-23 04:57:58.789Z | 321.859° NNW |
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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