LEMUR-2 CLARA, 68483
Orbit data source: Space-Track
LEMUR-2 CLARA, 68483 is a payload satellite owned by Spire (LU) 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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68483 intel report (Beta)
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Identifier
Orbit
Country
LU / LUXERelated business
Manufacturer
Spire/Glasgow
Mission
Operational spacecraft
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
7.6 kg wet, 7.6 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 0.2 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 LEMUR-2 CLARA
1 68483U 26067BV 26171.42951716 .00003314 00000-0 32625-3 0 9994
2 68483 97.7642 129.7686 0001235 292.7054 67.4035 14.92755284 12213Epoch: 2026-06-20T10:18Z
TLE epoch observation values (Epoch: 2026-06-20T10:18:30.282Z)
Latitude
0°
Longitude
66.49816°
Altitude
592.061 km
Speed
7.564 km/s
True Right ascension
08h 39m 04s
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
13:49:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
587.227 km
Perigee altitude
585.507 km
Semi-major axis
6,964.504 km
Eccentricity
0.00012
Inclination
97.7642°
RAAN
129.7686°
Arg. of periapsis
292.7054°
True anomaly
67.41657°
Mean anomaly
67.4035°
Eccentric anomaly
67.41003°
Mean motion
3.73429 °/min
Orbital period
96.4 mins
BSTAR
0.00032625
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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.LEMUR-2 CLARA 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-22 09:32:26.896Z | 37.4° NE | 2026-06-22 09:35:26.896Z | 96.584° ESE | 28.808° | 2026-06-22 09:38:26.896Z | 156.924° SSE |
| 4 mins | 2026-06-22 11:09:26.896Z | 316.579° NNW | 2026-06-22 11:10:26.896Z | 298.344° NW | 18.01° | 2026-06-22 11:13:26.896Z | 249.669° W |
| 4 mins | 2026-06-22 20:23:26.896Z | 99.048° ESE | 2026-06-22 20:25:26.896Z | 59.028° ENE | 20.13° | 2026-06-22 20:27:26.896Z | 25.561° NE |
| 5 mins | 2026-06-22 21:58:26.896Z | 220.86° SW | 2026-06-22 22:00:26.896Z | 266.016° W | 25.606° | 2026-06-22 22:03:26.896Z | 320.138° NNW |
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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