LEMUR-2 CALLUM-K-J, 67366
Orbit data source: Space-Track
LEMUR-2 CALLUM-K-J, 67366 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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67366 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Com/MetRO
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
Box + 2 Pan, 0.3 m
Radar Cross Section
0.054 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 LEMUR-2 CALLUM-K-J
1 67366U 26004D 26263.98585922 .00002155 00000-0 23535-3 0 9991
2 67366 97.8081 261.1434 0008687 169.2869 190.8535 14.88905170 37547Epoch: 2026-09-20T23:39Z
TLE epoch observation values (Epoch: 2026-09-20T23:39:38.236Z)
Latitude
-0°
Longitude
-93.6381°
Altitude
610.347 km
Speed
7.551 km/s
True Right ascension
17h 24m 34s
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
11:31:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
604.44 km
Perigee altitude
592.319 km
Semi-major axis
6,976.517 km
Eccentricity
0.00087
Inclination
97.8081°
RAAN
261.1434°
Arg. of periapsis
169.2869°
True anomaly
190.83478°
Mean anomaly
190.8535°
Eccentric anomaly
190.84414°
Mean motion
3.72465 °/min
Orbital period
96.65 mins
BSTAR
0.00023535
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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 CALLUM-K-J 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 | 2026-09-21 23:58:20.032Z | 168.873° S | 2026-09-22 00:02:20.032Z | 322.707° NNW | 76.301° | 2026-09-22 00:05:20.032Z | 345.61° N |
| 6 mins | 2026-09-22 13:20:20.032Z | 343.454° N | 2026-09-22 13:22:20.032Z | 296.539° NW | 38.558° | 2026-09-22 13:26:20.032Z | 220.181° SW |
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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