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 spacecraft
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
Unknown shape, 0.2 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 LEMUR-2 MARIO-SOUSA
1 67365U 26004C 26095.57017295 .00006521 00000-0 71692-3 0 9999
2 67365 97.8002 95.2766 0009187 31.3523 328.8239 14.87921196 12491Epoch: 2026-04-05T13:41Z
TLE epoch observation values (Epoch: 2026-04-05T13:41:02.942Z)
Latitude
-0.00011°
Longitude
56.14066°
Altitude
601.979 km
Speed
7.562 km/s
True Right ascension
06h 21m 06s
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
01:00:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
607.87 km
Perigee altitude
595.045 km
Semi-major axis
6,979.595 km
Eccentricity
0.00092
Inclination
97.8002°
RAAN
95.2766°
Arg. of periapsis
31.3523°
True anomaly
328.76935°
Mean anomaly
328.8239°
Eccentric anomaly
328.79663°
Mean motion
3.72218 °/min
Orbital period
96.72 mins
BSTAR
0.00071692
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-04-05 23:29:44.903Z | 141.838° SSE | 2026-04-05 23:32:44.903Z | 93.255° ESE | 33.43° | 2026-04-05 23:36:44.903Z | 3.571° NNE |
| 6 mins | 2026-04-06 12:51:44.903Z | 10.76° NNE | 2026-04-06 12:54:44.903Z | 204.443° SW | 43.041° | 2026-04-06 12:57:44.903Z | 195.434° 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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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