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, 0.3 m
Radar Cross Section
0.063 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 LEMUR-2 JULIA-JOEL
1 68476U 26067BN 26217.40819903 .00002516 00000-0 24702-3 0 9996
2 68476 97.7588 175.0275 0003857 93.2422 266.9239 14.93073199 19079Epoch: 2026-08-05T09:47Z
TLE epoch observation values (Epoch: 2026-08-05T09:47:48.396Z)
Latitude
0.00001°
Longitude
74.11282°
Altitude
591.549 km
Speed
7.564 km/s
True Right ascension
11h 40m 06s
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
16:18:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
588.063 km
Perigee altitude
582.691 km
Semi-major axis
6,963.514 km
Eccentricity
0.00039
Inclination
97.7588°
RAAN
175.0275°
Arg. of periapsis
93.2422°
True anomaly
266.87977°
Mean anomaly
266.9239°
Eccentric anomaly
266.90183°
Mean motion
3.73509 °/min
Orbital period
96.38 mins
BSTAR
0.00024702
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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 | 2026-08-06 10:30:17.919Z | 350.021° N | 2026-08-06 10:32:17.919Z | 295.871° NW | 36.921° | 2026-08-06 10:36:17.919Z | 212.396° SW |
| 6 mins | 2026-08-06 21:19:17.919Z | 170.798° S | 2026-08-06 21:21:17.919Z | 190.279° SSW | 43.702° | 2026-08-06 21:25:17.919Z | 345.757° N |
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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