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MARS-1, 68830

Orbit data source: Space-Track

MARS-1, 68830 is an American payload satellite in SSO that was launched on Mon, 30 Mar 2026 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
68830, 2026-067CW
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
LUOUT
Mission
Operational Commercial Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
~5 kg wet, ~5 kg dry
Launch date (UTC)
2026-03-30 (6 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 13 hours ago

TLE from 13 hours ago
0 MARS-1
1 68830U 26067CW  26263.15136256  .00004681  00000-0  21998-3 0  9995
2 68830  97.4624 220.4592 0004200 116.8630 243.3035 15.20084084 66918
Epoch: 2026-09-20T03:37Z
TLE epoch observation values (Epoch: 2026-09-20T03:37:57.725Z)
Latitude
0.00002°
Longitude
166.91902°
Altitude
509.976 km
Speed
7.608 km/s
True Right ascension
14h 41m 50s
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
09:42:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
505.445 km
Perigee altitude
499.665 km
Semi-major axis
6,880.692 km
Eccentricity
0.00042
Inclination
97.4624°
RAAN
220.4592°
Arg. of periapsis
116.863°
True anomaly
243.26051°
Mean anomaly
243.3035°
Eccentric anomaly
243.28201°
Mean motion
3.80273 °/min
Orbital period
94.67 mins
BSTAR
0.00021998
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