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: 16 hours ago
TLE from 16 hours ago
0 LEMUR-2 DELOITTE-3
1 68471U 26067BH 26228.44431647 .00002831 00000-0 28462-3 0 9999
2 68471 97.7623 185.6828 0003046 180.4993 179.6224 14.92015870 20715Epoch: 2026-08-16T10:39Z
TLE epoch observation values (Epoch: 2026-08-16T10:39:48.943Z)
Latitude
0.00007°
Longitude
60.88811°
Altitude
596.816 km
Speed
7.56 km/s
True Right ascension
12h 22m 43s
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
16:57:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.791 km
Perigee altitude
586.547 km
Semi-major axis
6,966.806 km
Eccentricity
0.0003
Inclination
97.7623°
RAAN
185.6828°
Arg. of periapsis
180.4993°
True anomaly
179.62263°
Mean anomaly
179.6224°
Eccentric anomaly
179.62251°
Mean motion
3.73244 °/min
Orbital period
96.45 mins
BSTAR
0.00028462
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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 | 2026-08-17 09:45:31.016Z | 23.399° NE | 2026-08-17 09:49:31.016Z | 101.727° ESE | 37.674° | 2026-08-17 09:52:31.016Z | 171.644° S |
| 5 mins | 2026-08-17 20:37:31.016Z | 112.256° ESE | 2026-08-17 20:39:31.016Z | 61.372° ENE | 27.449° | 2026-08-17 20:42:31.016Z | 10.708° NNE |
| 4 mins | 2026-08-17 22:13:31.016Z | 242.06° WSW | 2026-08-17 22:14:31.016Z | 260.604° W | 18.416° | 2026-08-17 22:17:31.016Z | 309.982° NW |
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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