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: 2 days ago
TLE from 2 days ago
0 SERT3
1 68499U 26067CM 26258.62220028 .00001350 00000-0 13944-3 0 9995
2 68499 97.7673 215.4295 0002911 94.5444 265.6108 14.91774966 25209Epoch: 2026-09-15T14:55Z
TLE epoch observation values (Epoch: 2026-09-15T14:55:58.104Z)
Latitude
0.00006°
Longitude
-3.14811°
Altitude
595.598 km
Speed
7.562 km/s
True Right ascension
14h 21m 43s
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
07:11:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
591.448 km
Perigee altitude
587.392 km
Semi-major axis
6,967.557 km
Eccentricity
0.00029
Inclination
97.7673°
RAAN
215.4295°
Arg. of periapsis
94.5444°
True anomaly
265.57754°
Mean anomaly
265.6108°
Eccentric anomaly
265.59417°
Mean motion
3.73183 °/min
Orbital period
96.47 mins
BSTAR
0.00013944
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-09-17 20:13:14.142Z | 99.088° ESE | 2026-09-17 20:15:14.142Z | 65.479° ENE | 17.986° | 2026-09-17 20:17:14.142Z | 32.617° NE |
| 6 mins | 2026-09-17 21:48:14.142Z | 208.392° SW | 2026-09-17 21:50:14.142Z | 254.727° W | 36.032° | 2026-09-17 21:54:14.142Z | 329.572° NNW |
| 6 mins | 2026-09-18 09:31:14.142Z | 41.36° NE | 2026-09-18 09:34:14.142Z | 108.581° ESE | 32.641° | 2026-09-18 09:37:14.142Z | 159.696° S |
| 4 mins | 2026-09-18 11:07:14.142Z | 326.836° NNW | 2026-09-18 11:09:14.142Z | 291.986° WNW | 19.441° | 2026-09-18 11:11:14.142Z | 257.587° W |
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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