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). Payloads include a variety of satellites, spacecraft, and rockets 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)
ABS 6 (LMI 1) details
Identifier | |
Orbit | GEO |
Last TLE update | 15 hours ago |
Origin | |
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 | Payload Rocket body Debris |
Shape & HBR | Box + 2 Pan, 21 m |
Radar Cross Section | 18.290 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 15 hours ago
0 ABS 6 (LMI 1)
1 25924U 99053A 25035.68604058 -.00000117 00000-0 00000+0 0 9999
2 25924 0.0606 266.8589 0002804 46.8749 227.3232 1.00270895 92848
Epoch: 2025-02-04T16:27Z
Definitive object data (Epoch: 2025-02-04T16:27:53.906Z)
Latitude | -0.04275° |
Longitude | 158.99565° |
Altitude | 35,794.384 km |
Speed | 3.074 km/s |
True Right ascension | 12h 04m 13s |
True Declination | 0° 02' 34" |
Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
Latitude | 0.02971° |
Longitude | 18.17606° |
Altitude | 35,785.615 km |
Speed | 3.075 km/s |
Apparent Right ascension | 02h 14m 53s |
Apparent Declination | -5° 23' 13" |
Sunlit | Object is in daylight |
Visualization observer readout
Local Sidereal Time | 09:04:16 |
Azimuth | 273.8° WNW |
Elevation | -12.916° |
Doppler factor | 1 |
Orbital elements
Apogee altitude | 35,799.738 km |
Perigee altitude | 35,776.091 km |
Semi-major axis | 42,166.052 km |
Eccentricity | 0.0002804 |
Inclination | 0.0606° |
RAAN | 266.8589° |
Arg. of periapsis | 46.8749° |
True anomaly | 227.29958° |
Mean anomaly | 227.3232° |
Eccentric anomaly | 227.31139° |
Mean motion | 0.25067 °/min |
BSTAR | Unknown |
Orbital period | 1436.16 mins |
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25924 neighbors
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Other satellites on launch #53 in the year 1999 (1999-09-26 UTC)
ABS 6 (LMI 1), 25924 |
SL-12 R/B(1), 25925 (Decayed) |
SL-12 PLAT, 25926 (Decayed) |
SL-12 R/B(2), 25927 |
ABS 6 (LMI 1) Visibility forecast
Observer location: undefined°, undefined
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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