LEMUR-2 JULIA-JOEL, 68476
Orbit data source: Space-Track
LEMUR-2 JULIA-JOEL, 68476 is a payload satellite owned by Spire (LU) 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
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: 8 hours ago
TLE from 8 hours ago
0 LEMUR-2 JULIA-JOEL
1 68476U 26067BN 26263.51261889 .00002335 00000-0 22831-3 0 9993
2 68476 97.7667 220.5376 0001575 7.1071 353.0170 14.93309065 25954Epoch: 2026-09-20T12:18Z
TLE epoch observation values (Epoch: 2026-09-20T12:18:10.272Z)
Latitude
-0.00006°
Longitude
36.58908°
Altitude
589.581 km
Speed
7.566 km/s
True Right ascension
14h 42m 09s
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
12:54:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
585.74 km
Perigee altitude
583.547 km
Semi-major axis
6,962.78 km
Eccentricity
0.00016
Inclination
97.7667°
RAAN
220.5376°
Arg. of periapsis
7.1071°
True anomaly
353.01481°
Mean anomaly
353.017°
Eccentric anomaly
353.0159°
Mean motion
3.73568 °/min
Orbital period
96.37 mins
BSTAR
0.00022831
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-09-20 20:29:22.523Z | 118.913° SE | 2026-09-20 20:32:22.523Z | 61.96° ENE | 25.581° | 2026-09-20 20:35:22.523Z | 14.334° NNE |
| 5 mins | 2026-09-20 22:05:22.523Z | 223.775° SW | 2026-09-20 22:07:22.523Z | 262.479° W | 24.043° | 2026-09-20 22:10:22.523Z | 315.17° NNW |
| 6 mins | 2026-09-21 09:47:22.523Z | 29.793° NE | 2026-09-21 09:50:22.523Z | 111.087° ESE | 49.465° | 2026-09-21 09:53:22.523Z | 172.226° S |
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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