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
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 LEMUR-2 KATIE
1 67387U 26004AA 26146.53044412 .00003320 00000-0 35108-3 0 9993
2 67387 97.8036 145.8174 0003911 137.8754 222.2765 14.89871102 20082Epoch: 2026-05-26T12:43Z
TLE epoch observation values (Epoch: 2026-05-26T12:43:50.371Z)
Latitude
-0.00003°
Longitude
70.75497°
Altitude
603.396 km
Speed
7.557 km/s
True Right ascension
09h 43m 16s
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
04:33:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
598.089 km
Perigee altitude
592.634 km
Semi-major axis
6,973.498 km
Eccentricity
0.00039
Inclination
97.8036°
RAAN
145.8174°
Arg. of periapsis
137.8754°
True anomaly
222.24636°
Mean anomaly
222.2765°
Eccentric anomaly
222.26143°
Mean motion
3.72707 °/min
Orbital period
96.59 mins
BSTAR
0.00035108
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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 | 2026-05-27 00:09:04.875Z | 180.302° SSW | 2026-05-27 00:11:04.875Z | 218.448° SW | 41.439° | 2026-05-27 00:15:04.875Z | 340.914° N |
| 4 mins | 2026-05-27 11:54:04.875Z | 64.454° ENE | 2026-05-27 11:56:04.875Z | 100.988° ESE | 18.09° | 2026-05-27 11:58:04.875Z | 133.301° SE |
| 6 mins | 2026-05-27 13:29:04.875Z | 340.806° N | 2026-05-27 13:31:04.875Z | 300.3° NW | 27.767° | 2026-05-27 13:35:04.875Z | 226.44° WSW |
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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