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: 15 hours ago
TLE from 15 hours ago
0 LEMUR-2 DELOITTE-3
1 68471U 26067BH 26217.44548338 .00003108 00000-0 31236-3 0 9994
2 68471 97.7606 174.8479 0002007 230.2291 129.8751 14.91966929 19077Epoch: 2026-08-05T10:41Z
TLE epoch observation values (Epoch: 2026-08-05T10:41:29.764Z)
Latitude
-0.00003°
Longitude
60.47411°
Altitude
595.742 km
Speed
7.561 km/s
True Right ascension
11h 39m 23s
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
15:22:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.22 km
Perigee altitude
587.423 km
Semi-major axis
6,966.959 km
Eccentricity
0.0002
Inclination
97.7606°
RAAN
174.8479°
Arg. of periapsis
230.2291°
True anomaly
129.89275°
Mean anomaly
129.8751°
Eccentric anomaly
129.88392°
Mean motion
3.73232 °/min
Orbital period
96.45 mins
BSTAR
0.00031236
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-08-06 09:47:09.625Z | 22.269° NNE | 2026-08-06 09:51:09.625Z | 97.789° ESE | 38.67° | 2026-08-06 09:55:09.625Z | 177.447° S |
| 5 mins | 2026-08-06 20:39:09.625Z | 114.985° SE | 2026-08-06 20:41:09.625Z | 63.454° ENE | 28.446° | 2026-08-06 20:44:09.625Z | 10.465° NNE |
| 4 mins | 2026-08-06 22:15:09.625Z | 241.353° WSW | 2026-08-06 22:16:09.625Z | 259.158° W | 17.646° | 2026-08-06 22:19:09.625Z | 308.328° NW |
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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