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
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 LEMUR-2 GRAM-E-SUE
1 67370U 26004H 26145.98282723 .00001975 00000-0 21921-3 0 9994
2 67370 97.7975 144.8887 0006075 206.0932 153.9979 14.88353461 19993Epoch: 2026-05-25T23:35Z
TLE epoch observation values (Epoch: 2026-05-25T23:35:16.272Z)
Latitude
-0.00008°
Longitude
-92.49189°
Altitude
609.929 km
Speed
7.552 km/s
True Right ascension
09h 39m 33s
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
03:35:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
604.344 km
Perigee altitude
595.866 km
Semi-major axis
6,978.242 km
Eccentricity
0.00061
Inclination
97.7975°
RAAN
144.8887°
Arg. of periapsis
206.0932°
True anomaly
154.0284°
Mean anomaly
153.9979°
Eccentric anomaly
154.01315°
Mean motion
3.72327 °/min
Orbital period
96.69 mins
BSTAR
0.00021921
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-05-26 23:54:57.603Z | 165.196° S | 2026-05-26 23:57:57.603Z | 155.722° SSE | 44.153° | 2026-05-27 00:01:57.603Z | 348.334° N |
| 6 mins | 2026-05-27 13:16:57.603Z | 344.974° N | 2026-05-27 13:18:57.603Z | 292.919° NW | 34.192° | 2026-05-27 13:22:57.603Z | 216.737° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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