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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 (4 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: 17 hours ago

TLE from 17 hours ago
0 MERCURY ONE (M1)
1 66742U 25276CE  26092.45688124  .00006985  00000-0  33724-3 0  9994
2 66742  97.4233 167.3090 0001497 193.7038 166.4156 15.18969597 18922
Epoch: 2026-04-02T10:57Z
TLE epoch observation values (Epoch: 2026-04-02T10:57:54.539Z)
Latitude
-0.00001°
Longitude
172.02666°
Altitude
513.044 km
Speed
7.607 km/s
True Right ascension
11h 09m 14s
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
09:52:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
506.952 km
Perigee altitude
504.891 km
Semi-major axis
6,884.058 km
Eccentricity
0.00015
Inclination
97.4233°
RAAN
167.309°
Arg. of periapsis
193.7038°
True anomaly
166.41963°
Mean anomaly
166.4156°
Eccentric anomaly
166.41761°
Mean motion
3.79994 °/min
Orbital period
94.74 mins
BSTAR
0.00033724
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