LEMUR-2 MARIO-SOUSA, 67365
Orbit data source: Space-Track
LEMUR-2 MARIO-SOUSA, 67365 is a payload satellite owned by Spire/Lux (US) in SSO that was launched on Sun, 11 Jan 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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67365 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Com/MetRO
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
4.6 kg wet, 4.6 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.2 m
Radar Cross Section
0.054 m²
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 LEMUR-2 MARIO-SOUSA
1 67365U 26004C 26146.53816729 .00004769 00000-0 52117-3 0 9994
2 67365 97.7988 145.4298 0007538 200.8484 159.2427 14.88309484 20077Epoch: 2026-05-26T12:54Z
TLE epoch observation values (Epoch: 2026-05-26T12:54:57.653Z)
Latitude
0.00001°
Longitude
67.57941°
Altitude
611.176 km
Speed
7.551 km/s
True Right ascension
09h 41m 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
04:33:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
605.503 km
Perigee altitude
594.982 km
Semi-major axis
6,978.379 km
Eccentricity
0.00075
Inclination
97.7988°
RAAN
145.4298°
Arg. of periapsis
200.8484°
True anomaly
159.27329°
Mean anomaly
159.2427°
Eccentric anomaly
159.258°
Mean motion
3.72316 °/min
Orbital period
96.69 mins
BSTAR
0.00052117
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Other satellites on launch #4 in the year 2026 (2026-01-11 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.LEMUR-2 MARIO-SOUSA 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 | 2026-05-26 22:46:09.020Z | 91.563° ESE | 2026-05-26 22:48:09.020Z | 60.682° ENE | 14.374° | 2026-05-26 22:50:09.020Z | 31.942° NE |
| 6 mins | 2026-05-27 00:21:09.020Z | 200.001° SSW | 2026-05-27 00:23:09.020Z | 255.691° W | 36.079° | 2026-05-27 00:27:09.020Z | 334.495° NNW |
| 5 mins | 2026-05-27 12:06:09.020Z | 51.976° ENE | 2026-05-27 12:08:09.020Z | 93.013° ESE | 24.785° | 2026-05-27 12:11:09.020Z | 149.295° SSE |
| 5 mins | 2026-05-27 13:42:09.020Z | 326.168° NNW | 2026-05-27 13:44:09.020Z | 286.214° WNW | 21.463° | 2026-05-27 13:47:09.020Z | 239.661° WSW |
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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