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, 0.3 m
Radar Cross Section
0.054 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 LEMUR-2 HCS-BAZUS
1 67388U 26004AB 26264.09371556 .00002664 00000-0 27719-3 0 9997
2 67388 97.8090 261.9522 0004023 112.8156 247.3487 14.90699645 37599Epoch: 2026-09-21T02:14Z
TLE epoch observation values (Epoch: 2026-09-21T02:14:57.024Z)
Latitude
-0.00005°
Longitude
-131.76388°
Altitude
599.873 km
Speed
7.559 km/s
True Right ascension
17h 27m 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
12:35:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
595.58 km
Perigee altitude
589.971 km
Semi-major axis
6,970.912 km
Eccentricity
0.0004
Inclination
97.809°
RAAN
261.9522°
Arg. of periapsis
112.8156°
True anomaly
247.30616°
Mean anomaly
247.3487°
Eccentric anomaly
247.32743°
Mean motion
3.72914 °/min
Orbital period
96.54 mins
BSTAR
0.00027719
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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 | 2026-09-21 23:19:18.920Z | 131.817° SE | 2026-09-21 23:23:18.920Z | 57.332° ENE | 30.528° | 2026-09-21 23:26:18.920Z | 10.014° NNE |
| 4 mins | 2026-09-22 00:57:18.920Z | 242.919° WSW | 2026-09-22 00:58:18.920Z | 261.867° W | 20.051° | 2026-09-22 01:01:18.920Z | 310.949° NW |
| 7 mins | 2026-09-22 12:39:18.920Z | 21.877° NNE | 2026-09-22 12:42:18.920Z | 96.049° ESE | 64.458° | 2026-09-22 12:46:18.920Z | 183.009° 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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