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MERCURY ONE (M1), 66742

Orbit data source: Space-Track

MERCURY ONE (M1), 66742 is an American payload satellite in SSO that was launched on Fri, 28 Nov 2025 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
66742, 2025-276CE
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
PROTE
Mission
Operational Commercial Technology
Bus & Motor
M1, Unknown motor
Mass
50 kg wet, 50 kg dry
Launch date (UTC)
2025-11-28 (6 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.4 m
Radar Cross Section
0.400 m²

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

TLE from 12 hours ago
0 MERCURY ONE (M1)
1 66742U 25276CE  26141.19821853  .00003044  00000-0  14712-3 0  9997
2 66742  97.4196 215.2020 0003842  79.5405 280.6263 15.19368550 26325
Epoch: 2026-05-21T04:45Z
TLE epoch observation values (Epoch: 2026-05-21T04:45:26.080Z)
Latitude
-0.00001°
Longitude
-95.00353°
Altitude
510.35 km
Speed
7.609 km/s
True Right ascension
14h 20m 48s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
02:08:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
507.359 km
Perigee altitude
502.071 km
Semi-major axis
6,882.852 km
Eccentricity
0.00038
Inclination
97.4196°
RAAN
215.202°
Arg. of periapsis
79.5405°
True anomaly
280.58303°
Mean anomaly
280.6263°
Eccentric anomaly
280.60466°
Mean motion
3.80094 °/min
Orbital period
94.71 mins
BSTAR
0.00014712
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