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 Commercial Com/MetRO
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
Box + 2 Pan, 0.5 m
Radar Cross Section
0.063 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 LEMUR-2 CLARA
1 68483U 26067BV 26262.30839543 .00002736 00000-0 26693-3 0 9990
2 68483 97.7746 219.5126 0003033 11.5425 348.5863 14.93261743 25772Epoch: 2026-09-19T07:24Z
TLE epoch observation values (Epoch: 2026-09-19T07:24:05.365Z)
Latitude
-0.00006°
Longitude
110.27146°
Altitude
588.745 km
Speed
7.567 km/s
True Right ascension
14h 38m 03s
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
06:57:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
586.903 km
Perigee altitude
582.679 km
Semi-major axis
6,962.928 km
Eccentricity
0.0003
Inclination
97.7746°
RAAN
219.5126°
Arg. of periapsis
11.5425°
True anomaly
348.57942°
Mean anomaly
348.5863°
Eccentric anomaly
348.58286°
Mean motion
3.73556 °/min
Orbital period
96.37 mins
BSTAR
0.00026693
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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 | 2026-09-20 20:31:42.764Z | 124.534° SE | 2026-09-20 20:34:42.764Z | 72.824° E | 27.086° | 2026-09-20 20:37:42.764Z | 17.169° NNE |
| 4 mins | 2026-09-20 22:08:42.764Z | 233.679° WSW | 2026-09-20 22:10:42.764Z | 275.131° WNW | 22.365° | 2026-09-20 22:12:42.764Z | 309.291° NW |
| 6 mins | 2026-09-21 09:50:42.764Z | 32.445° NE | 2026-09-21 09:52:42.764Z | 85.395° E | 52.278° | 2026-09-21 09:56:42.764Z | 176.664° S |
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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