LEMUR-2 DELOITTE-2, 68491
Orbit data source: Space-Track
LEMUR-2 DELOITTE-2, 68491 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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68491 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, 0.3 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 LEMUR-2 DELOITTE-2
1 68491U 26067CD 26171.42878380 .00005420 00000-0 54666-3 0 9997
2 68491 97.7562 129.5381 0004525 60.7715 299.3955 14.91508220 12206Epoch: 2026-06-20T10:17Z
TLE epoch observation values (Epoch: 2026-06-20T10:17:26.920Z)
Latitude
-0.00008°
Longitude
66.5324°
Altitude
594.726 km
Speed
7.563 km/s
True Right ascension
08h 38m 09s
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
12:36:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
593.404 km
Perigee altitude
587.098 km
Semi-major axis
6,968.388 km
Eccentricity
0.00045
Inclination
97.7562°
RAAN
129.5381°
Arg. of periapsis
60.7715°
True anomaly
299.35031°
Mean anomaly
299.3955°
Eccentric anomaly
299.37291°
Mean motion
3.73117 °/min
Orbital period
96.48 mins
BSTAR
0.00054666
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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-2 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 | 2026-06-22 09:33:23.339Z | 33.662° NE | 2026-06-22 09:36:23.339Z | 86.185° E | 29.767° | 2026-06-22 09:40:23.339Z | 163.856° S |
| 4 mins | 2026-06-22 11:10:23.339Z | 321.857° NNW | 2026-06-22 11:12:23.339Z | 286.584° WNW | 17.189° | 2026-06-22 11:14:23.339Z | 255.224° W |
| 4 mins | 2026-06-22 20:25:23.339Z | 98.126° ESE | 2026-06-22 20:26:23.339Z | 78.087° E | 21.276° | 2026-06-22 20:29:23.339Z | 22.799° NE |
| 5 mins | 2026-06-22 22:00:23.339Z | 223.817° SW | 2026-06-22 22:02:23.339Z | 267.368° W | 24.164° | 2026-06-22 22:05:23.339Z | 319.199° NNW |
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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