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 spacecraft
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
10 kg wet, 10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 0.2 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 LEMUR-2 DELOITTE-3
1 68471U 26067BH 26171.43123884 .00001875 00000-0 19239-3 0 9995
2 68471 97.7579 129.5495 0005292 56.8162 303.3564 14.91594119 12217Epoch: 2026-06-20T10:20Z
TLE epoch observation values (Epoch: 2026-06-20T10:20:59.035Z)
Latitude
0°
Longitude
65.65756°
Altitude
593.978 km
Speed
7.564 km/s
True Right ascension
08h 38m 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
07:17:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
593.671 km
Perigee altitude
586.296 km
Semi-major axis
6,968.12 km
Eccentricity
0.00053
Inclination
97.7579°
RAAN
129.5495°
Arg. of periapsis
56.8162°
True anomaly
303.30573°
Mean anomaly
303.3564°
Eccentric anomaly
303.33107°
Mean motion
3.73138 °/min
Orbital period
96.48 mins
BSTAR
0.00019239
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-20 21:44:16.444Z | 194.558° SSW | 2026-06-20 21:47:16.444Z | 246.062° WSW | 31.543° | 2026-06-20 21:51:16.444Z | 329.888° NNW |
| 5 mins | 2026-06-21 09:29:16.444Z | 53.006° ENE | 2026-06-21 09:31:16.444Z | 100.54° ESE | 26.98° | 2026-06-21 09:34:16.444Z | 155.353° SSE |
| 4 mins | 2026-06-21 11:05:16.444Z | 316.606° NNW | 2026-06-21 11:06:16.444Z | 297.398° NW | 19.382° | 2026-06-21 11:09:16.444Z | 247.212° WSW |
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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