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
None
Manufacturer
Unknown
Mission
Operational spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 1.1 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 LEMUR-2 DELOITTE-2
1 68491U 26067CD 26127.14630705 .00003573 00000-0 36468-3 0 9991
2 68491 97.7543 85.9950 0003229 158.5091 201.6264 14.91250893 5600Epoch: 2026-05-07T03:30Z
TLE epoch observation values (Epoch: 2026-05-07T03:30:40.929Z)
Latitude
0.00004°
Longitude
168.32782°
Altitude
599.169 km
Speed
7.559 km/s
True Right ascension
05h 43m 58s
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
01:03:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
593.304 km
Perigee altitude
588.803 km
Semi-major axis
6,969.19 km
Eccentricity
0.00032
Inclination
97.7543°
RAAN
85.995°
Arg. of periapsis
158.5091°
True anomaly
201.61277°
Mean anomaly
201.6264°
Eccentric anomaly
201.61958°
Mean motion
3.73052 °/min
Orbital period
96.5 mins
BSTAR
0.00036468
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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 | 2026-05-07 21:20:41.943Z | 172.095° S | 2026-05-07 21:24:41.943Z | 313.211° NW | 42.842° | 2026-05-07 21:27:41.943Z | 343.649° N |
| 5 mins | 2026-05-08 10:41:41.943Z | 336.047° NNW | 2026-05-08 10:43:41.943Z | 281.344° WNW | 30.562° | 2026-05-08 10:46:41.943Z | 225.391° WSW |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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