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 spacecraft
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
Unknown shape, 0.2 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 LEMUR-2 EMARCHIA
1 68492U 26067CE 26171.42575653 .00004929 00000-0 49505-3 0 9994
2 68492 97.7562 129.5443 0005155 60.6651 299.5083 14.91718315 12206Epoch: 2026-06-20T10:13Z
TLE epoch observation values (Epoch: 2026-06-20T10:13:05.364Z)
Latitude
0.00008°
Longitude
67.63138°
Altitude
593.85 km
Speed
7.564 km/s
True Right ascension
08h 38m 10s
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
13:50:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
593.188 km
Perigee altitude
586.004 km
Semi-major axis
6,967.733 km
Eccentricity
0.00052
Inclination
97.7562°
RAAN
129.5443°
Arg. of periapsis
60.6651°
True anomaly
299.45687°
Mean anomaly
299.5083°
Eccentric anomaly
299.48259°
Mean motion
3.73169 °/min
Orbital period
96.47 mins
BSTAR
0.00049505
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-22 09:28:32.155Z | 35.16° NE | 2026-06-22 09:31:32.155Z | 83.305° E | 26.89° | 2026-06-22 09:35:32.155Z | 159.228° S |
| 4 mins | 2026-06-22 11:05:32.155Z | 325.503° NNW | 2026-06-22 11:07:32.155Z | 288.79° WNW | 19.08° | 2026-06-22 11:09:32.155Z | 254.453° W |
| 4 mins | 2026-06-22 20:20:32.155Z | 96.811° ESE | 2026-06-22 20:22:32.155Z | 57.751° ENE | 19.179° | 2026-06-22 20:24:32.155Z | 25.533° NE |
| 5 mins | 2026-06-22 21:55:32.155Z | 219.42° SW | 2026-06-22 21:57:32.155Z | 266.467° W | 26.654° | 2026-06-22 22:00:32.155Z | 321.372° 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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