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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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Identifier
67365, 2026-004C
Orbit
SSO
Country
Flag of USUS
Related 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)
2026-01-11 (4 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 0.2 m
Radar Cross Section
0.054 m²

Expand to show TLE details & history
Last 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 19993
Epoch: 2026-05-26T00:00Z
TLE epoch observation values (Epoch: 2026-05-26T00:00:26.975Z)
Latitude
Longitude
-98.79193°
Altitude
611.092 km
Speed
7.551 km/s
True Right ascension
09h 39m 36s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
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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