ASIASTAR, 26107
Orbit data source: Space-Track
ASIASTAR, 26107 is a payload satellite owned by Worldspace (US) in GEO that was launched on Tue, 21 Mar 2000 UTC via an ARIANE 5G launch vehicle from the French Guiana (FRGUI). 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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26107 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Astrium/Toulouse
Mission
Operational Commercial Communications
Bus & Motor
EUROSTAR 2000+, R-4D-11-300
Mass
2,777 kg wet, 1,220 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 14.0 m
Radar Cross Section
18.564 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 ASIASTAR
1 26107U 00016A 26093.34137468 -.00000333 00000-0 00000-0 0 9999
2 26107 8.9580 58.9426 0005048 323.1985 37.4478 1.00272359 95174Epoch: 2026-04-03T08:11Z
TLE epoch observation values (Epoch: 2026-04-03T08:11:34.772Z)
Latitude
0.10406°
Longitude
105.04991°
Altitude
35,768.971 km
Speed
3.076 km/s
True Right ascension
03h 58m 29s
True Declination
0° 06' 14"
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
03:20:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,808.752 km
Perigee altitude
35,766.181 km
Semi-major axis
42,165.603 km
Eccentricity
0.0005
Inclination
8.958°
RAAN
58.9426°
Arg. of periapsis
323.1985°
True anomaly
37.48299°
Mean anomaly
37.4478°
Eccentric anomaly
37.46539°
Mean motion
0.25067 °/min
Orbital period
1,436.14 mins
BSTAR
0
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Other satellites on launch #16 in the year 2000 (2000-03-21 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.ASIASTAR 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. |
|---|---|---|---|---|---|---|---|
| ASIASTAR is likely not visible in the next few days. |
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26107 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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