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USA 24, 18010

Orbit data source: Space-Track

USA 24, 18010 is an American payload satellite in LEO that was launched on Fri, 15 May 1987 UTC via an ATLAS H launch vehicle from the Air Force Western Test Range (AFWTR). 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
18010, 1987-043F
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
Martin Marietta
Mission
Defense Sigint
Bus & Motor
NOSS SSU, Unknown motor
Mass
200 kg wet, 200 kg dry
Launch date (UTC)
1987-05-15 (39 years ago)
Launch vehicle
ATLAS H
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 1 Ant, 5.0 m
Radar Cross Section
1.051 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 USA 24
1 18010U 87043F   26171.47204903  .00010170  00000-0  59719-3 0  9991
2 18010  63.2987 349.8221 0786278 104.6637 264.2847 13.86723300345919
Epoch: 2026-06-20T11:19Z
TLE epoch observation values (Epoch: 2026-06-20T11:19:45.036Z)
Latitude
0.00004°
Longitude
-88.80171°
Altitude
1,043.365 km
Speed
7.28 km/s
True Right ascension
23h 19m 17s
True Declination
0° 00' 00"
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
00:39:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,514.27 km
Perigee altitude
363.618 km
Semi-major axis
7,317.081 km
Eccentricity
0.07863
Inclination
63.2987°
RAAN
349.8221°
Arg. of periapsis
104.6637°
True anomaly
255.44153°
Mean anomaly
264.2847°
Eccentric anomaly
259.85016°
Mean motion
3.46766 °/min
Orbital period
103.82 mins
BSTAR
0.00059719
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