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 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: 2 days ago
TLE from 2 days ago
0 LEMUR-2 DELOITTE-2
1 68491U 26067CD 26258.62017706 .00004388 00000-0 43578-3 0 9994
2 68491 97.7653 215.3964 0004498 101.1712 259.0013 14.92230077 25209Epoch: 2026-09-15T14:53Z
TLE epoch observation values (Epoch: 2026-09-15T14:53:03.297Z)
Latitude
-0.00004°
Longitude
-2.45084°
Altitude
594.625 km
Speed
7.562 km/s
True Right ascension
14h 21m 35s
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
03:00:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
591.136 km
Perigee altitude
584.869 km
Semi-major axis
6,966.139 km
Eccentricity
0.00045
Inclination
97.7653°
RAAN
215.3964°
Arg. of periapsis
101.1712°
True anomaly
258.95071°
Mean anomaly
259.0013°
Eccentric anomaly
258.976°
Mean motion
3.73297 °/min
Orbital period
96.44 mins
BSTAR
0.00043578
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-09-17 10:53:54.803Z | 342.543° N | 2026-09-17 10:56:54.803Z | 289.55° WNW | 25.75° | 2026-09-17 10:59:54.803Z | 237.875° WSW |
| 4 mins | 2026-09-17 20:09:54.803Z | 90.002° ESE | 2026-09-17 20:10:54.803Z | 73.676° E | 16.186° | 2026-09-17 20:13:54.803Z | 27.481° NE |
| 6 mins | 2026-09-17 21:43:54.803Z | 199.957° SSW | 2026-09-17 21:46:54.803Z | 275.728° WNW | 39.149° | 2026-09-17 21:49:54.803Z | 328.976° NNW |
| 5 mins | 2026-09-18 09:27:54.803Z | 54.355° ENE | 2026-09-18 09:29:54.803Z | 101.67° ESE | 29.765° | 2026-09-18 09:32:54.803Z | 154.957° SSE |
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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