LEMUR-2 GRAM-E-SUE, 67370
Orbit data source: Space-Track
LEMUR-2 GRAM-E-SUE, 67370 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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67370 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: 12 hours ago
TLE from 12 hours ago
0 LEMUR-2 GRAM-E-SUE
1 67370U 26004H 26264.21760888 .00002851 00000-0 30927-3 0 9995
2 67370 97.8046 261.3225 0006923 175.1423 184.9862 14.88934101 37583Epoch: 2026-09-21T05:13Z
TLE epoch observation values (Epoch: 2026-09-21T05:13:21.407Z)
Latitude
-0.00005°
Longitude
-177.11729°
Altitude
609.116 km
Speed
7.552 km/s
True Right ascension
17h 25m 17s
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
10:30:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
603.119 km
Perigee altitude
593.46 km
Semi-major axis
6,976.426 km
Eccentricity
0.00069
Inclination
97.8046°
RAAN
261.3225°
Arg. of periapsis
175.1423°
True anomaly
184.97931°
Mean anomaly
184.9862°
Eccentric anomaly
184.98275°
Mean motion
3.72472 °/min
Orbital period
96.65 mins
BSTAR
0.00030927
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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 GRAM-E-SUE 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 | 2026-09-21 23:06:10.656Z | 121.827° SE | 2026-09-21 23:09:10.656Z | 74.527° E | 24.653° | 2026-09-21 23:12:10.656Z | 20.512° NNE |
| 5 mins | 2026-09-22 00:43:10.656Z | 225.041° WSW | 2026-09-22 00:45:10.656Z | 267.335° W | 26.378° | 2026-09-22 00:48:10.656Z | 318.279° NNW |
| 6 mins | 2026-09-22 12:27:10.656Z | 31.806° NE | 2026-09-22 12:30:10.656Z | 118.768° SE | 47.533° | 2026-09-22 12:33:10.656Z | 172.362° S |
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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