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, 0.2 m
Radar Cross Section
0.063 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 LEMUR-2 CLARA
1 68483U 26067BV 26220.15659985 .00001827 00000-0 18096-3 0 9995
2 68483 97.7671 177.8642 0004759 106.8005 253.3737 14.93044967 19487Epoch: 2026-08-08T03:45Z
TLE epoch observation values (Epoch: 2026-08-08T03:45:30.227Z)
Latitude
0.00002°
Longitude
164.81627°
Altitude
592.441 km
Speed
7.563 km/s
True Right ascension
11h 51m 27s
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
00:05:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
588.779 km
Perigee altitude
582.151 km
Semi-major axis
6,963.602 km
Eccentricity
0.00048
Inclination
97.7671°
RAAN
177.8642°
Arg. of periapsis
106.8005°
True anomaly
253.32145°
Mean anomaly
253.3737°
Eccentric anomaly
253.34758°
Mean motion
3.73501 °/min
Orbital period
96.39 mins
BSTAR
0.00018096
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-08-08 10:45:01.320Z | 350.391° N | 2026-08-08 10:48:01.320Z | 300.267° NW | 27.915° | 2026-08-08 10:52:01.320Z | 225.678° WSW |
| 6 mins | 2026-08-08 21:35:01.320Z | 188.798° SSW | 2026-08-08 21:38:01.320Z | 280.422° WNW | 38.017° | 2026-08-08 21:41:01.320Z | 335.104° NNW |
| 4 mins | 2026-08-09 09:19:01.320Z | 66.384° ENE | 2026-08-09 09:20:01.320Z | 86.286° E | 20.661° | 2026-08-09 09:23:01.320Z | 140.939° SSE |
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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