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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68830 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
LUOUT
Mission
Operational Commercial Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
~5 kg wet, ~5 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 MARS-1
1 68830U 26067CW 26259.13581350 .00006005 00000-0 28156-3 0 9992
2 68830 97.4623 216.4864 0003970 124.8705 235.2903 15.20046096 66307Epoch: 2026-09-16T03:15Z
TLE epoch observation values (Epoch: 2026-09-16T03:15:34.286Z)
Latitude
-0.00009°
Longitude
172.50181°
Altitude
510.347 km
Speed
7.608 km/s
True Right ascension
14h 25m 56s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
03:01:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
505.401 km
Perigee altitude
499.938 km
Semi-major axis
6,880.807 km
Eccentricity
0.0004
Inclination
97.4623°
RAAN
216.4864°
Arg. of periapsis
124.8705°
True anomaly
235.25291°
Mean anomaly
235.2903°
Eccentric anomaly
235.27161°
Mean motion
3.80263 °/min
Orbital period
94.67 mins
BSTAR
0.00028156
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Other satellites on launch #67 in the year 2026 (2026-03-30 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.MARS-1 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-09-17 20:30:03.105Z | 100.319° ESE | 2026-09-17 20:31:03.105Z | 79.711° E | 20.419° | 2026-09-17 20:34:03.105Z | 22.468° NNE |
| 4 mins | 2026-09-17 22:04:03.105Z | 236.357° WSW | 2026-09-17 22:05:03.105Z | 260.159° W | 23.271° | 2026-09-17 22:08:03.105Z | 317.346° NNW |
| 4 mins | 2026-09-18 09:34:03.105Z | 55.17° ENE | 2026-09-18 09:36:03.105Z | 110.955° ESE | 28.682° | 2026-09-18 09:38:03.105Z | 151.632° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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