LEMUR-2 DELOITTE-3, 68471
Orbit data source: Space-Track
LEMUR-2 DELOITTE-3, 68471 is an American 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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68471 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Com/MetRO
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
10 kg wet, 10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 LEMUR-2 DELOITTE-3
1 68471U 26067BH 26307.63386498 .00003205 00000-0 31704-3 0 9990
2 68471 97.7760 263.7962 0002805 337.0906 23.0187 14.92581308 32526Epoch: 2026-11-03T15:12Z
TLE epoch observation values (Epoch: 2026-11-03T15:12:45.934Z)
Latitude
-0.00007°
Longitude
-7.2889°
Altitude
591.133 km
Speed
7.565 km/s
True Right ascension
17h 35m 11s
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
12:24:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
588.863 km
Perigee altitude
584.955 km
Semi-major axis
6,965.046 km
Eccentricity
0.00028
Inclination
97.776°
RAAN
263.7962°
Arg. of periapsis
337.0906°
True anomaly
23.03127°
Mean anomaly
23.0187°
Eccentric anomaly
23.02499°
Mean motion
3.73385 °/min
Orbital period
96.42 mins
BSTAR
0.00031704
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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 DELOITTE-3 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 | 2026-11-04 20:19:10.495Z | 114.359° SE | 2026-11-04 20:22:10.495Z | 65.331° ENE | 20.926° | 2026-11-04 20:25:10.495Z | 19.077° NNE |
| 5 mins | 2026-11-04 21:55:10.495Z | 214.913° SW | 2026-11-04 21:57:10.495Z | 257.525° W | 30.256° | 2026-11-04 22:00:10.495Z | 318.46° NNW |
| 6 mins | 2026-11-05 09:38:10.495Z | 41.494° NE | 2026-11-05 09:40:10.495Z | 88.502° E | 38.828° | 2026-11-05 09:44:10.495Z | 167.322° S |
| 4 mins | 2026-11-05 11:14:10.495Z | 318.237° NNW | 2026-11-05 11:15:10.495Z | 301.8° NW | 16.621° | 2026-11-05 11:18:10.495Z | 255.029° W |
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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