LEMUR-2 KATIE, 67387
Orbit data source: Space-Track
LEMUR-2 KATIE, 67387 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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67387 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Spire/Glasgow
Mission
Operational spacecraft
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
Unknown shape, 0.2 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 LEMUR-2 KATIE
1 67387U 26004AA 26095.28126454 .00008308 00000-0 87683-3 0 9991
2 67387 97.8052 95.2325 0002768 11.9174 348.2109 14.89524089 12455Epoch: 2026-04-05T06:45Z
TLE epoch observation values (Epoch: 2026-04-05T06:45:01.256Z)
Latitude
0.00005°
Longitude
160.38832°
Altitude
600.568 km
Speed
7.56 km/s
True Right ascension
06h 20m 55s
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
19:28:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
598.376 km
Perigee altitude
594.515 km
Semi-major axis
6,974.582 km
Eccentricity
0.00028
Inclination
97.8052°
RAAN
95.2325°
Arg. of periapsis
11.9174°
True anomaly
348.20442°
Mean anomaly
348.2109°
Eccentric anomaly
348.20766°
Mean motion
3.7262 °/min
Orbital period
96.61 mins
BSTAR
0.00087683
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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 KATIE 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 | 2026-04-05 13:45:58.715Z | 335.959° NNW | 2026-04-05 13:48:58.715Z | 283.733° WNW | 19.914° | 2026-04-05 13:50:58.715Z | 250.535° W |
| 5 mins | 2026-04-05 23:01:58.715Z | 104.533° ESE | 2026-04-05 23:03:58.715Z | 69.317° E | 19.479° | 2026-04-05 23:06:58.715Z | 21.171° NNE |
| 6 mins | 2026-04-06 00:36:58.715Z | 209.723° SW | 2026-04-06 00:39:58.715Z | 275.189° WNW | 26.848° | 2026-04-06 00:42:58.715Z | 324.101° NNW |
| 5 mins | 2026-04-06 12:21:58.715Z | 44.351° NE | 2026-04-06 12:23:58.715Z | 97.731° ESE | 32.714° | 2026-04-06 12:26:58.715Z | 162.681° 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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