SERT3, 68499
Orbit data source: Space-Track
SERT3, 68499 is a payload satellite owned by Muon Space (US) 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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68499 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Muon Space
Mission
Operational Commercial Technology
Bus & Motor
MUON HALO, Unknown motor
Mass
130 kg wet, 125 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 2.6 m
Radar Cross Section
2.173 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 SERT3
1 68499U 26067CM 26307.85348723 .00000920 00000-0 96519-4 0 9990
2 68499 97.7766 263.9759 0001042 29.4966 330.6311 14.91913820 32543Epoch: 2026-11-03T20:29Z
TLE epoch observation values (Epoch: 2026-11-03T20:29:01.296Z)
Latitude
-0.00008°
Longitude
-86.38968°
Altitude
594.377 km
Speed
7.563 km/s
True Right ascension
17h 35m 54s
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
11:12:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
589.714 km
Perigee altitude
588.262 km
Semi-major axis
6,967.125 km
Eccentricity
0.0001
Inclination
97.7766°
RAAN
263.9759°
Arg. of periapsis
29.4966°
True anomaly
330.62524°
Mean anomaly
330.6311°
Eccentric anomaly
330.62817°
Mean motion
3.73218 °/min
Orbital period
96.46 mins
BSTAR
0.000096519
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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.SERT3 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-11-04 20:45:30.166Z | 139.175° SSE | 2026-11-04 20:48:30.166Z | 87.155° E | 39.518° | 2026-11-04 20:52:30.166Z | 4.226° NNE |
| 6 mins | 2026-11-05 10:05:30.166Z | 14.983° NNE | 2026-11-05 10:07:30.166Z | 31.262° NE | 75.056° | 2026-11-05 10:11:30.166Z | 191.503° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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