LEMUR-2 JULIA-JOEL, 68476
Orbit data source: Space-Track
LEMUR-2 JULIA-JOEL, 68476 is a Luxembourger 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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68476 intel report (Beta)
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Identifier
Orbit
Country
LU / LUXERelated 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: 19 hours ago
TLE from 19 hours ago
0 LEMUR-2 JULIA-JOEL
1 68476U 26067BN 26126.84856262 .00003584 00000-0 35503-3 0 9999
2 68476 97.7548 85.7685 0003840 63.4149 296.7463 14.92444235 5565Epoch: 2026-05-06T20:21Z
TLE epoch observation values (Epoch: 2026-05-06T20:21:55.810Z)
Latitude
-0.00005°
Longitude
-84.4172°
Altitude
592.156 km
Speed
7.565 km/s
True Right ascension
05h 43m 04s
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
23:12:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.009 km
Perigee altitude
584.66 km
Semi-major axis
6,965.472 km
Eccentricity
0.00038
Inclination
97.7548°
RAAN
85.7685°
Arg. of periapsis
63.4149°
True anomaly
296.707°
Mean anomaly
296.7463°
Eccentric anomaly
296.72665°
Mean motion
3.73351 °/min
Orbital period
96.42 mins
BSTAR
0.00035503
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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 JULIA-JOEL 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 | 2026-05-07 20:37:53.449Z | 133.495° SE | 2026-05-07 20:41:53.449Z | 56.722° ENE | 27.623° | 2026-05-07 20:44:53.449Z | 9.014° NNE |
| 4 mins | 2026-05-07 22:15:53.449Z | 245.433° WSW | 2026-05-07 22:16:53.449Z | 264.051° W | 17.811° | 2026-05-07 22:19:53.449Z | 311.298° NW |
| 7 mins | 2026-05-08 09:56:53.449Z | 20.634° NNE | 2026-05-08 09:59:53.449Z | 91.552° ESE | 42.546° | 2026-05-08 10:03:53.449Z | 184.058° SSW |
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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