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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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Iframe URL

https://www.satcat.com/sats-embedded/25924?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

25924, 1999-053A

Orbit

GEO

Country

AE / ABS

Related business

ABS Global Ltd. (US)

Manufacturer

LMCSS

Mission

Operational Commercial Communications

Bus & Motor

A2100, LEROS 1C

Mass

3,740 kg wet, 1,730 kg dry

Launch date (UTC)

1999-09-26 (27 years ago)

Launch vehicle

PROTON-K/DM-2M

Launch site

Tyuratam Missile And Space Complex (TTMTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Box + 2 Pan, 10.5 m

Radar Cross Section

18.290 m², Large (>1 m²)

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Last TLE update: 12 hours ago

TLE from 12 hours ago

0 ABS 6 (LMI 1)
1 25924U 99053A   26257.89175395 -.00000126  00000-0  00000-0 0  9997
2 25924   0.0224 237.3162 0001678 257.2793 339.3070  1.00272590 98742

Epoch: 2026-09-14T21:24Z

TLE epoch observation values (Epoch: 2026-09-14T21:24:07.541Z)

Latitude

-0.03143°

Longitude

158.99279°

Altitude

35,779.252 km

Speed

3.075 km/s

True Right ascension

07h 35m 33s

True Declination

0° 01' 53"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

Unknown

Longitude

Unknown

Altitude

Unknown

Speed

Unknown

Apparent Right ascension

Unknown

Apparent Declination

Unknown

Sunlit

N/A

Visualization observer readout

Local Sidereal Time

02:29:39

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

35,794.515 km

Perigee altitude

35,780.364 km

Semi-major axis

42,165.577 km

Eccentricity

0.00017

Inclination

0.0224°

RAAN

237.3162°

Arg. of periapsis

257.2793°

True anomaly

339.3002°

Mean anomaly

339.307°

Eccentric anomaly

339.3036°

Mean motion

0.25067 °/min

Orbital period

1,436.14 mins

BSTAR

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Other satellites on launch #53 in the year 1999 (1999-09-26 UTC)

SL-12 R/B(2), 25927

SL-12 R/B(1), 25925 (Decayed)

SL-12 PLAT, 25926 (Decayed)

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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.

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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.
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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

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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings

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Check out ABS 6 (LMI 1), 25924 on other resources

View ABS 6 (LMI 1), 25924 on NASA - NSSDCA Website

View ABS 6 (LMI 1), 25924 on Heavens-Above

View ABS 6 (LMI 1), 25924 on Keep Track

View ABS 6 (LMI 1), 25924 on Celestrak

View ABS 6 (LMI 1), 25924 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

ABS 6 (LMI 1), 25924

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 12 hours ago

TLE from 12 hours ago

TLE epoch observation values (Epoch: 2026-09-14T21:24:07.541Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #53 in the year 1999 (1999-09-26 UTC)

ABS 6 (LMI 1) Visibility

25924 neighbors

Co-orbital & Co-planar RSOs

Check out ABS 6 (LMI 1), 25924 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 12 hours ago