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, 0.1 m
Radar Cross Section
0.054 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 LEMUR-2 GRAM-E-SUE
1 67370U 26004H 26206.55072091 .00002814 00000-0 30761-3 0 9995
2 67370 97.7990 204.5080 0007868 32.6453 327.5249 14.88629817 29004Epoch: 2026-07-25T13:13Z
TLE epoch observation values (Epoch: 2026-07-25T13:13:02.286Z)
Latitude
-0.00002°
Longitude
62.98709°
Altitude
600.619 km
Speed
7.562 km/s
True Right ascension
13h 38m 01s
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
11:11:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
604.73 km
Perigee altitude
593.751 km
Semi-major axis
6,977.378 km
Eccentricity
0.00079
Inclination
97.799°
RAAN
204.508°
Arg. of periapsis
32.6453°
True anomaly
327.47645°
Mean anomaly
327.5249°
Eccentric anomaly
327.50068°
Mean motion
3.72396 °/min
Orbital period
96.67 mins
BSTAR
0.00030761
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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 | 2026-07-25 23:02:35.639Z | 115.292° SE | 2026-07-25 23:05:35.639Z | 64.531° ENE | 20.616° | 2026-07-25 23:08:35.639Z | 17.893° NNE |
| 6 mins | 2026-07-26 00:38:35.639Z | 214.039° SW | 2026-07-26 00:40:35.639Z | 252.014° W | 25.253° | 2026-07-26 00:44:35.639Z | 323.842° NNW |
| 6 mins | 2026-07-26 12:23:35.639Z | 38.418° NE | 2026-07-26 12:25:35.639Z | 87.23° E | 34.517° | 2026-07-26 12:29:35.639Z | 170.525° 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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