LEMUR-2 HCS-BAZUS, 67388
Orbit data source: Space-Track
LEMUR-2 HCS-BAZUS, 67388 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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67388 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 HCS-BAZUS
1 67388U 26004AB 26146.52943412 .00004823 00000-0 50771-3 0 9993
2 67388 97.8022 145.8007 0003669 131.1990 228.9545 14.89836454 20082Epoch: 2026-05-26T12:42Z
TLE epoch observation values (Epoch: 2026-05-26T12:42:23.107Z)
Latitude
0.00001°
Longitude
71.10286°
Altitude
603.166 km
Speed
7.557 km/s
True Right ascension
09h 43m 12s
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
05:28:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
598.028 km
Perigee altitude
592.911 km
Semi-major axis
6,973.607 km
Eccentricity
0.00037
Inclination
97.8022°
RAAN
145.8007°
Arg. of periapsis
131.199°
True anomaly
228.9228°
Mean anomaly
228.9545°
Eccentric anomaly
228.93865°
Mean motion
3.72698 °/min
Orbital period
96.59 mins
BSTAR
0.00050771
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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 HCS-BAZUS 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 | 2026-05-27 00:06:38.729Z | 175.303° S | 2026-05-27 00:09:38.729Z | 213.591° SW | 41.841° | 2026-05-27 00:13:38.729Z | 341.753° N |
| 4 mins | 2026-05-27 11:52:38.729Z | 64.571° ENE | 2026-05-27 11:54:38.729Z | 100.321° ESE | 17.577° | 2026-05-27 11:56:38.729Z | 132.249° SE |
| 6 mins | 2026-05-27 13:27:38.729Z | 341.957° N | 2026-05-27 13:29:38.729Z | 301.534° NW | 28.384° | 2026-05-27 13:33:38.729Z | 225.647° WSW |
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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