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 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, 0.2 m
Radar Cross Section
0.054 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 LEMUR-2 KATIE
1 67387U 26004AA 26206.42891562 .00004544 00000-0 47298-3 0 9996
2 67387 97.8051 204.9737 0002523 7.5432 352.5824 14.90324027 29000Epoch: 2026-07-25T10:17Z
TLE epoch observation values (Epoch: 2026-07-25T10:17:38.309Z)
Latitude
0.00004°
Longitude
107.42274°
Altitude
598.217 km
Speed
7.562 km/s
True Right ascension
13h 39m 53s
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
10:26:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
595.706 km
Perigee altitude
592.188 km
Semi-major axis
6,972.084 km
Eccentricity
0.00025
Inclination
97.8051°
RAAN
204.9737°
Arg. of periapsis
7.5432°
True anomaly
352.57867°
Mean anomaly
352.5824°
Eccentric anomaly
352.58053°
Mean motion
3.7282 °/min
Orbital period
96.56 mins
BSTAR
0.00047298
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-07-25 23:19:08.985Z | 130.396° SE | 2026-07-25 23:22:08.985Z | 79.849° E | 27.238° | 2026-07-25 23:25:08.985Z | 16.386° NNE |
| 5 mins | 2026-07-26 00:56:08.985Z | 230.603° WSW | 2026-07-26 00:58:08.985Z | 265.917° W | 18.776° | 2026-07-26 01:01:08.985Z | 312.93° NW |
| 7 mins | 2026-07-26 12:39:08.985Z | 21.882° NNE | 2026-07-26 12:42:08.985Z | 101.167° ESE | 42.212° | 2026-07-26 12:46:08.985Z | 183.387° SSW |
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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