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: 18 hours ago
TLE from 18 hours ago
0 LEMUR-2 MARIO-SOUSA
1 67365U 26004C 26146.00031222 .00004465 00000-0 48839-3 0 9992
2 67365 97.7989 144.9005 0007491 202.9157 157.1727 14.88304144 19993Epoch: 2026-05-26T00:00Z
TLE epoch observation values (Epoch: 2026-05-26T00:00:26.975Z)
Latitude
0°
Longitude
-98.79193°
Altitude
611.092 km
Speed
7.551 km/s
True Right ascension
09h 39m 36s
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
03:36:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
605.487 km
Perigee altitude
595.032 km
Semi-major axis
6,978.396 km
Eccentricity
0.00075
Inclination
97.7989°
RAAN
144.9005°
Arg. of periapsis
202.9157°
True anomaly
157.20597°
Mean anomaly
157.1727°
Eccentric anomaly
157.18934°
Mean motion
3.72314 °/min
Orbital period
96.69 mins
BSTAR
0.00048839
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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 22:45:39.606Z | 97.7° ESE | 2026-05-26 22:47:39.606Z | 68.732° E | 14.396° | 2026-05-26 22:49:39.606Z | 38.004° NE |
| 6 mins | 2026-05-27 00:20:39.606Z | 194.993° SSW | 2026-05-27 00:23:39.606Z | 279.308° WNW | 35.38° | 2026-05-27 00:26:39.606Z | 332.05° NNW |
| 5 mins | 2026-05-27 12:06:39.606Z | 59.848° ENE | 2026-05-27 12:08:39.606Z | 106.128° ESE | 24.491° | 2026-05-27 12:11:39.606Z | 153.874° SSE |
| 5 mins | 2026-05-27 13:41:39.606Z | 332.991° NNW | 2026-05-27 13:43:39.606Z | 297.198° NW | 21.456° | 2026-05-27 13:46:39.606Z | 244.344° 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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