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, 1.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 3 days ago
TLE from 3 days ago
0 LEMUR-2 JULIA-JOEL
1 68476U 26067BN 26154.46989715 .00004050 00000-0 39861-3 0 9998
2 68476 97.7559 112.9768 0001482 1.7080 358.4144 14.92632898 9684Epoch: 2026-06-03T11:16Z
TLE epoch observation values (Epoch: 2026-06-03T11:16:39.113Z)
Latitude
-0.00005°
Longitude
51.88578°
Altitude
591.74 km
Speed
7.565 km/s
True Right ascension
07h 31m 54s
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
02:31:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
587.779 km
Perigee altitude
585.715 km
Semi-major axis
6,964.884 km
Eccentricity
0.00015
Inclination
97.7559°
RAAN
112.9768°
Arg. of periapsis
1.708°
True anomaly
358.41393°
Mean anomaly
358.4144°
Eccentric anomaly
358.41417°
Mean motion
3.73398 °/min
Orbital period
96.41 mins
BSTAR
0.00039861
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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 | 2026-06-06 21:27:36.909Z | 180.191° SSW | 2026-06-06 21:30:36.909Z | 272.359° WNW | 41.998° | 2026-06-06 21:33:36.909Z | 338.76° N |
| 4 mins | 2026-06-07 09:11:36.909Z | 62.351° ENE | 2026-06-07 09:13:36.909Z | 98.59° ESE | 18.237° | 2026-06-07 09:15:36.909Z | 132.002° SE |
| 5 mins | 2026-06-07 10:46:36.909Z | 339.964° N | 2026-06-07 10:48:36.909Z | 298.688° NW | 27.547° | 2026-06-07 10:51:36.909Z | 234.283° WSW |
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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