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, 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 HCS-BAZUS
1 67388U 26004AB 26206.42722800 .00003807 00000-0 39725-3 0 9992
2 67388 97.8040 204.9492 0002050 8.6967 351.4286 14.90321727 29001Epoch: 2026-07-25T10:15Z
TLE epoch observation values (Epoch: 2026-07-25T10:15:12.499Z)
Latitude
-0.00001°
Longitude
108.00746°
Altitude
598.556 km
Speed
7.561 km/s
True Right ascension
13h 39m 47s
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
10:25:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
595.384 km
Perigee altitude
592.525 km
Semi-major axis
6,972.091 km
Eccentricity
0.00021
Inclination
97.804°
RAAN
204.9492°
Arg. of periapsis
8.6967°
True anomaly
351.4251°
Mean anomaly
351.4286°
Eccentric anomaly
351.42685°
Mean motion
3.72819 °/min
Orbital period
96.56 mins
BSTAR
0.00039725
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-07-25 23:17:26.976Z | 122.372° SE | 2026-07-25 23:20:26.976Z | 59.875° ENE | 25.992° | 2026-07-25 23:23:26.976Z | 11.478° NNE |
| 4 mins | 2026-07-26 00:54:26.976Z | 240.35° WSW | 2026-07-26 00:55:26.976Z | 259.671° W | 19.651° | 2026-07-26 00:58:26.976Z | 310.833° NW |
| 6 mins | 2026-07-26 12:37:26.976Z | 27.696° NE | 2026-07-26 12:39:26.976Z | 78.31° E | 40.575° | 2026-07-26 12:43:26.976Z | 180.574° 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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