LEMUR-2 EMARCHIA, 68492
Orbit data source: Space-Track
LEMUR-2 EMARCHIA, 68492 is a payload satellite owned by Spire (DE) in SSO that was launched on Mon, 30 Mar 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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68492 intel report (Beta)
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Identifier
Orbit
Country
DE / GERRelated business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Com/MetRO
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
7.6 kg wet, 7.6 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.2 m
Radar Cross Section
0.063 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 LEMUR-2 EMARCHIA
1 68492U 26067CE 26217.43441134 .00004311 00000-0 42893-3 0 9990
2 68492 97.7588 174.8411 0001469 234.0930 126.0153 14.92163900 19061Epoch: 2026-08-05T10:25Z
TLE epoch observation values (Epoch: 2026-08-05T10:25:33.139Z)
Latitude
-0.00002°
Longitude
64.46416°
Altitude
594.834 km
Speed
7.562 km/s
True Right ascension
11h 39m 21s
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
19:45:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
589.231 km
Perigee altitude
587.185 km
Semi-major axis
6,966.345 km
Eccentricity
0.00015
Inclination
97.7588°
RAAN
174.8411°
Arg. of periapsis
234.093°
True anomaly
126.02891°
Mean anomaly
126.0153°
Eccentric anomaly
126.02211°
Mean motion
3.73281 °/min
Orbital period
96.44 mins
BSTAR
0.00042893
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Other satellites on launch #67 in the year 2026 (2026-03-30 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 EMARCHIA 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 | 2026-08-06 09:32:01.713Z | 35.777° NE | 2026-08-06 09:35:01.713Z | 92.153° ESE | 29.228° | 2026-08-06 09:38:01.713Z | 156.381° SSE |
| 4 mins | 2026-08-06 11:09:01.713Z | 319.089° NNW | 2026-08-06 11:10:01.713Z | 301.587° NW | 17.562° | 2026-08-06 11:13:01.713Z | 252.023° W |
| 5 mins | 2026-08-06 20:23:01.713Z | 105.517° ESE | 2026-08-06 20:25:01.713Z | 67.461° ENE | 20.935° | 2026-08-06 20:28:01.713Z | 18.745° NNE |
| 5 mins | 2026-08-06 21:58:01.713Z | 215.777° SW | 2026-08-06 22:00:01.713Z | 254.573° W | 24.864° | 2026-08-06 22:03:01.713Z | 315.251° NNW |
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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