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 Amateur Astronomy
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, 0.1 m
Radar Cross Section
0.072 m²
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 LEMUR-2 CALLUM-K-J
1 67366U 26004D 26146.54888429 .00004714 00000-0 51846-3 0 9990
2 67366 97.8014 145.4531 0008093 195.4133 164.6838 14.88049508 20070Epoch: 2026-05-26T13:10Z
TLE epoch observation values (Epoch: 2026-05-26T13:10:23.602Z)
Latitude
-0.00007°
Longitude
63.73403°
Altitude
612.517 km
Speed
7.55 km/s
True Right ascension
09h 41m 48s
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
04:32:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
606.704 km
Perigee altitude
595.408 km
Semi-major axis
6,979.193 km
Eccentricity
0.00081
Inclination
97.8014°
RAAN
145.4531°
Arg. of periapsis
195.4133°
True anomaly
164.70827°
Mean anomaly
164.6838°
Eccentric anomaly
164.69604°
Mean motion
3.72251 °/min
Orbital period
96.71 mins
BSTAR
0.00051846
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-05-26 23:00:33.606Z | 110.286° ESE | 2026-05-26 23:03:33.606Z | 58.319° ENE | 19.619° | 2026-05-26 23:05:33.606Z | 26.097° NE |
| 5 mins | 2026-05-27 00:36:33.606Z | 215.594° SW | 2026-05-27 00:38:33.606Z | 259.179° W | 27.387° | 2026-05-27 00:41:33.606Z | 319.036° NNW |
| 6 mins | 2026-05-27 12:21:33.606Z | 40.127° NE | 2026-05-27 12:23:33.606Z | 87.396° E | 33.049° | 2026-05-27 12:27:33.606Z | 168.511° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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