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CHECKMATE 8, 56162

Orbit data source: Space-Track

CHECKMATE 8, 56162 is a payload satellite owned by SDA (US) in LEO that was launched on Sun, 02 Apr 2023 UTC via an FALCON 9 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
56162, 2023-050A
Orbit
LEO
Last TLE update
16 hours ago
Origin
Manufacturer
York Space Sys
Mission
Operational Defense Communications
Bus & Motor
S-CLASS, Unknown motor
Mass
~300 kg wet, ~300 kg dry
Launch date (UTC)
2023-04-02 (2 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 1 Pan, 1.0 m
Radar Cross Section
0.945 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 16 hours ago
0 CHECKMATE 8
1 56162U 23050A   25213.90476156  .00000100  00000-0  79126-4 0  9991
2 56162  81.0024  17.9586 0007207 101.6716 258.5249 13.84882258117958
Epoch: 2025-08-01T21:42Z
TLE epoch observation values (Epoch: 2025-08-01T21:42:51.398Z)
Latitude
-0.00006°
Longitude
101.49585°
Altitude
950.532 km
Speed
7.376 km/s
True Right ascension
01h 11m 50s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
80.47767°
Longitude
170.74526°
Altitude
954.835 km
Speed
7.384 km/s
Apparent Right ascension
14h 48m 54s
Apparent Declination
38° 23' 31"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
03:29:20
Azimuth
8.062° NNE
Elevation
-11.146°
Doppler factor
1
Orbital elements
Apogee altitude
949.117 km
Perigee altitude
938.563 km
Semi-major axis
7,321.977 km
Eccentricity
0.00072
Inclination
81.0024°
RAAN
17.9586°
Arg. of periapsis
101.6716°
True anomaly
258.44398°
Mean anomaly
258.5249°
Eccentric anomaly
258.48444°
Mean motion
3.46418 °/min
Orbital period
103.92 mins
BSTAR
0.000079126
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