ANGOSAT 1, 43087
Orbit data source: Space-Track
ANGOSAT 1, 43087 is a payload satellite owned by GGPEN (AO) in GEO that was launched on Tue, 26 Dec 2017 UTC via a ZENIT-3SLBF launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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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43087 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
AO / AGORelated business
Manufacturer
RKKE
Mission
Non-operational Civil Communications
Bus & Motor
YAMAL 100, Unknown motor
Mass
1,647 kg wet, ~1,400 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 6.0 m
Radar Cross Section
11.377 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 ANGOSAT 1
1 43087U 17086A 26004.81730104 -.00000114 00000-0 00000+0 0 9996
2 43087 7.1697 69.1954 0021280 175.9259 159.3388 0.99382805 29102Epoch: 2026-01-04T19:36Z
TLE epoch observation values (Epoch: 2026-01-04T19:36:54.809Z)
Latitude
-2.9862°
Longitude
6.08564°
Altitude
36,122.012 km
Speed
3.059 km/s
True Right ascension
02h 58m 56s
True Declination
-2° 58' 60"
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
02:12:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,128.967 km
Perigee altitude
35,948.441 km
Semi-major axis
42,416.841 km
Eccentricity
0.00213
Inclination
7.1697°
RAAN
69.1954°
Arg. of periapsis
175.9259°
True anomaly
159.42463°
Mean anomaly
159.3388°
Eccentric anomaly
159.38173°
Mean motion
0.24845 °/min
Orbital period
1,448.99 mins
BSTAR
0
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Other satellites on launch #86 in the year 2017 (2017-12-26 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.ANGOSAT 1 Visibility
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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. |
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| ANGOSAT 1 is likely not visible in the next few days. |
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43087 neighbors
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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