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 spacecraft
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
Unknown shape, 0.1 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 LEMUR-2 GRAM-E-SUE
1 67370U 26004H 26095.48934660 .00004945 00000-0 54313-3 0 9998
2 67370 97.7988 95.2070 0008128 36.7679 323.4094 14.88083407 12486Epoch: 2026-04-05T11:44Z
TLE epoch observation values (Epoch: 2026-04-05T11:44:39.546Z)
Latitude
0.00002°
Longitude
85.24819°
Altitude
602.404 km
Speed
7.561 km/s
True Right ascension
06h 20m 49s
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
00:59:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
606.622 km
Perigee altitude
595.277 km
Semi-major axis
6,979.087 km
Eccentricity
0.00081
Inclination
97.7988°
RAAN
95.207°
Arg. of periapsis
36.7679°
True anomaly
323.35383°
Mean anomaly
323.4094°
Eccentric anomaly
323.38162°
Mean motion
3.72259 °/min
Orbital period
96.71 mins
BSTAR
0.00054313
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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 | 2026-04-05 23:10:57.048Z | 122.458° SE | 2026-04-05 23:13:57.048Z | 69.341° E | 24.195° | 2026-04-05 23:16:57.048Z | 16.463° NNE |
| 5 mins | 2026-04-06 00:47:57.048Z | 230.019° WSW | 2026-04-06 00:49:57.048Z | 270.9° WNW | 21.702° | 2026-04-06 00:52:57.048Z | 317.987° NNW |
| 6 mins | 2026-04-06 12:31:57.048Z | 27.31° NE | 2026-04-06 12:34:57.048Z | 113.072° SE | 39.285° | 2026-04-06 12:37:57.048Z | 175.406° 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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