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: 4 hours ago
TLE from 4 hours ago
0 LEMUR-2 CLARA
1 68483U 26067BV 26260.29812131 .00003424 00000-0 33266-3 0 9999
2 68483 97.7743 217.5251 0003183 16.9655 343.1670 14.93250970 25470Epoch: 2026-09-17T07:09Z
TLE epoch observation values (Epoch: 2026-09-17T07:09:17.681Z)
Latitude
-0.00004°
Longitude
113.96406°
Altitude
588.727 km
Speed
7.567 km/s
True Right ascension
14h 30m 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
04:06:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
587.041 km
Perigee altitude
582.608 km
Semi-major axis
6,962.961 km
Eccentricity
0.00032
Inclination
97.7743°
RAAN
217.5251°
Arg. of periapsis
16.9655°
True anomaly
343.15643°
Mean anomaly
343.167°
Eccentric anomaly
343.16172°
Mean motion
3.73553 °/min
Orbital period
96.37 mins
BSTAR
0.00033266
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-17 20:10:36.577Z | 103.522° ESE | 2026-09-17 20:12:36.577Z | 74.309° E | 15.989° | 2026-09-17 20:15:36.577Z | 27.913° NE |
| 6 mins | 2026-09-17 21:45:36.577Z | 199.981° SSW | 2026-09-17 21:48:36.577Z | 276.806° WNW | 39.069° | 2026-09-17 21:51:36.577Z | 329.273° NNW |
| 5 mins | 2026-09-18 09:28:36.577Z | 47.424° ENE | 2026-09-18 09:30:36.577Z | 87.067° E | 28.947° | 2026-09-18 09:33:36.577Z | 149.364° SSE |
| 4 mins | 2026-09-18 11:04:36.577Z | 323.418° NNW | 2026-09-18 11:06:36.577Z | 284.211° WNW | 21.382° | 2026-09-18 11:08:36.577Z | 250.404° W |
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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