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CXO, 25867

Orbit data source: Space-Track

CXO, 25867 is a payload satellite owned by NASA MSFC (US) in HEO that was launched on Fri, 23 Jul 1999 UTC via an SPACE SHUTTLE 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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Identifier
25867, 1999-040B
Orbit
HEO
Country
Flag of USUS
Related business
Manufacturer
TRW
Mission
Operational Civil Astronomy
Bus & Motor
AXAF, TR-308 X4
Mass
5,677 kg wet, 4,653 kg dry
Launch date (UTC)
1999-07-23 (26 years ago)
Launch vehicle
SPACE SHUTTLE
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 2 Pan, 9.8 m
Radar Cross Section
72.045 m², Large (>1 m²)

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Last TLE update: in 2 days

TLE from in 2 days
0 CXO
1 25867U 99040B   25304.30481514  .00000945  00000-0  00000-0 0  9998
2 25867  52.1821 124.1649 8211418 310.5885   0.2547  0.37801472 16457
Epoch: 2025-10-31T07:18Z
TLE epoch observation values (Epoch: 2025-10-31T07:18:56.028Z)
Latitude
-32.39959°
Longitude
-54.85715°
Altitude
8,081.541 km
Speed
7.087 km/s
True Right ascension
06h 18m 54s
True Declination
-32° 19' 23"
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
13:16:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
140,765.359 km
Perigee altitude
8,073.138 km
Semi-major axis
80,797.385 km
Eccentricity
0.82114
Inclination
52.1821°
RAAN
124.1649°
Arg. of periapsis
310.5885°
True anomaly
4.5397°
Mean anomaly
0.2547°
Eccentric anomaly
1.42336°
Mean motion
0.0945 °/min
Orbital period
3,809.39 mins
BSTAR
0
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