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 spacecraft
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
Unknown shape, 0.3 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 LEMUR-2 JULIA-JOEL
1 68476U 26067BN 26171.42953485 .00003530 00000-0 34714-3 0 9992
2 68476 97.7564 129.6907 0000656 202.9431 157.1759 14.92757515 12210Epoch: 2026-06-20T10:18Z
TLE epoch observation values (Epoch: 2026-06-20T10:18:31.811Z)
Latitude
-0.00001°
Longitude
66.41387°
Altitude
592.806 km
Speed
7.563 km/s
True Right ascension
08h 38m 45s
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
10:38:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
586.816 km
Perigee altitude
585.902 km
Semi-major axis
6,964.496 km
Eccentricity
0.00007
Inclination
97.7564°
RAAN
129.6907°
Arg. of periapsis
202.9431°
True anomaly
157.17882°
Mean anomaly
157.1759°
Eccentric anomaly
157.17736°
Mean motion
3.73429 °/min
Orbital period
96.4 mins
BSTAR
0.00034714
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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 | 2026-06-22 09:32:15.433Z | 35.485° NE | 2026-06-22 09:35:15.433Z | 90.019° ESE | 28.821° | 2026-06-22 09:38:15.433Z | 155.326° SSE |
| 4 mins | 2026-06-22 11:09:15.433Z | 319.755° NNW | 2026-06-22 11:10:15.433Z | 302.255° NW | 17.638° | 2026-06-22 11:13:15.433Z | 252.097° W |
| 4 mins | 2026-06-22 20:23:15.433Z | 102.444° ESE | 2026-06-22 20:25:15.433Z | 63.459° ENE | 20.47° | 2026-06-22 20:27:15.433Z | 27.989° NE |
| 5 mins | 2026-06-22 21:58:15.433Z | 218.082° SW | 2026-06-22 22:00:15.433Z | 260.348° W | 25.43° | 2026-06-22 22:03:15.433Z | 318.013° NNW |
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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