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, 0.5 m
Radar Cross Section
0.063 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 LEMUR-2 EMARCHIA
1 68492U 26067CE 26254.44739213 .00003626 00000-0 35915-3 0 9995
2 68492 97.7644 211.3198 0004908 111.8114 248.3628 14.92437581 24587Epoch: 2026-09-11T10:44Z
TLE epoch observation values (Epoch: 2026-09-11T10:44:14.680Z)
Latitude
0.00004°
Longitude
59.78801°
Altitude
594.643 km
Speed
7.562 km/s
True Right ascension
14h 05m 16s
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
15:02:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.775 km
Perigee altitude
583.937 km
Semi-major axis
6,965.493 km
Eccentricity
0.00049
Inclination
97.7644°
RAAN
211.3198°
Arg. of periapsis
111.8114°
True anomaly
248.31053°
Mean anomaly
248.3628°
Eccentric anomaly
248.33667°
Mean motion
3.73349 °/min
Orbital period
96.42 mins
BSTAR
0.00035915
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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 | 2026-09-12 09:50:04.085Z | 23.288° NE | 2026-09-12 09:53:04.085Z | 74.106° E | 53.885° | 2026-09-12 09:57:04.085Z | 178.147° S |
| 5 mins | 2026-09-12 20:41:04.085Z | 118.991° SE | 2026-09-12 20:43:04.085Z | 67.86° E | 34.696° | 2026-09-12 20:46:04.085Z | 10.554° NNE |
| 4 mins | 2026-09-12 22:17:04.085Z | 240.313° WSW | 2026-09-12 22:19:04.085Z | 275.828° WNW | 17.507° | 2026-09-12 22:21:04.085Z | 306.197° NW |
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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