LEMUR-2 EMARCHIA, 68492
Orbit data source: Space-Track
LEMUR-2 EMARCHIA, 68492 is a German payload satellite 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
None
Manufacturer
Unknown
Mission
Operational spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 1.1 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 LEMUR-2 EMARCHIA
1 68492U 26067CE 26127.14716967 .00004692 00000-0 47674-3 0 9991
2 68492 97.7546 85.9951 0003547 162.2208 197.9135 14.91279480 5607Epoch: 2026-05-07T03:31Z
TLE epoch observation values (Epoch: 2026-05-07T03:31:55.459Z)
Latitude
-0.00005°
Longitude
168.01654°
Altitude
599.34 km
Speed
7.559 km/s
True Right ascension
05h 43m 58s
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
01:58:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
593.436 km
Perigee altitude
588.492 km
Semi-major axis
6,969.101 km
Eccentricity
0.00035
Inclination
97.7546°
RAAN
85.9951°
Arg. of periapsis
162.2208°
True anomaly
197.901°
Mean anomaly
197.9135°
Eccentric anomaly
197.90725°
Mean motion
3.73059 °/min
Orbital period
96.5 mins
BSTAR
0.00047674
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-05-07 21:21:25.439Z | 172.485° S | 2026-05-07 21:25:25.439Z | 249.313° W | 43.921° | 2026-05-07 21:29:25.439Z | 343.733° N |
| 4 mins | 2026-05-08 09:07:25.439Z | 66.314° ENE | 2026-05-08 09:09:25.439Z | 101.218° ESE | 16.47° | 2026-05-08 09:11:25.439Z | 131.803° SE |
| 6 mins | 2026-05-08 10:42:25.439Z | 341.658° N | 2026-05-08 10:44:25.439Z | 297.305° NW | 29.809° | 2026-05-08 10:48:25.439Z | 222.873° SW |
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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