ABS 6 (LMI 1), 25924
Orbit data source: Space-Track
ABS 6 (LMI 1), 25924 is an Emirian payload satellite in GEO that was launched on Sun, 26 Sep 1999 UTC via a PROTON-K/DM-2M 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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25924 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
AE / ABSRelated business
Manufacturer
LMCSS
Mission
Operational Commercial Communications
Bus & Motor
A2100, LEROS 1C
Mass
3,740 kg wet, 1,730 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 10.5 m
Radar Cross Section
18.290 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 22 hours ago
TLE from 22 hours ago
0 ABS 6 (LMI 1)
1 25924U 99053A 25348.87598378 .00000000 00000-0 00000-0 0 9995
2 25924 0.0308 42.4151 0002941 246.0445 269.6858 1.00268441 95984Epoch: 2025-12-14T21:01Z
TLE epoch observation values (Epoch: 2025-12-14T21:01:24.998Z)
Latitude
0.00039°
Longitude
158.96466°
Altitude
35,787.048 km
Speed
3.075 km/s
True Right ascension
13h 12m 24s
True Declination
0° 00' 01"
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
17:23:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,801.004 km
Perigee altitude
35,776.202 km
Semi-major axis
42,166.74 km
Eccentricity
0.00029
Inclination
0.0308°
RAAN
42.4151°
Arg. of periapsis
246.0445°
True anomaly
269.6521°
Mean anomaly
269.6858°
Eccentric anomaly
269.66895°
Mean motion
0.25066 °/min
Orbital period
1,436.2 mins
BSTAR
0
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Other satellites on launch #53 in the year 1999 (1999-09-26 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.ABS 6 (LMI 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. |
|---|---|---|---|---|---|---|---|
| ABS 6 (LMI 1) is likely not visible in the next few days. |
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25924 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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