ABS 2A, 41588
Orbit data source: Space-Track
ABS 2A, 41588 is a payload satellite owned by ABS (HK) (AE) in GEO that was launched on Wed, 15 Jun 2016 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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41588 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
AE / ABSRelated business
Manufacturer
Boeing/ES
Mission
Operational Commercial Communications
Bus & Motor
BSS-702SP, XIPS-25
Mass
1,954 kg wet, ~1,500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 20.0 m
Radar Cross Section
33.227 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 ABS 2A
1 41588U 16038A 25354.99407935 .00000000 00000-0 00000-0 0 9999
2 41588 0.0275 5.8161 0001211 201.9587 314.6638 1.00267012 34928Epoch: 2025-12-20T23:51Z
TLE epoch observation values (Epoch: 2025-12-20T23:51:28.455Z)
Latitude
0.01955°
Longitude
74.73818°
Altitude
35,783.86 km
Speed
3.075 km/s
True Right ascension
10h 49m 40s
True Declination
0° 01' 10"
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
13:56:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,794.11 km
Perigee altitude
35,783.897 km
Semi-major axis
42,167.14 km
Eccentricity
0.00012
Inclination
0.0275°
RAAN
5.8161°
Arg. of periapsis
201.9587°
True anomaly
314.65393°
Mean anomaly
314.6638°
Eccentric anomaly
314.65886°
Mean motion
0.25066 °/min
Orbital period
1,436.22 mins
BSTAR
0
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Other satellites on launch #38 in the year 2016 (2016-06-15 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.ABS 2A 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. |
|---|---|---|---|---|---|---|---|
| ABS 2A is likely not visible in the next few days. |
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41588 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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