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: 14 hours ago
TLE from 14 hours ago
0 LEMUR-2 DELOITTE-2
1 68491U 26067CD 26263.11282319 .00003268 00000-0 32568-3 0 9991
2 68491 97.7660 219.8263 0004708 91.2286 268.9472 14.92264659 25871Epoch: 2026-09-20T02:42Z
TLE epoch observation values (Epoch: 2026-09-20T02:42:27.923Z)
Latitude
-0.00007°
Longitude
-179.80171°
Altitude
593.98 km
Speed
7.563 km/s
True Right ascension
14h 39m 18s
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
09:42:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
591.174 km
Perigee altitude
584.615 km
Semi-major axis
6,966.031 km
Eccentricity
0.00047
Inclination
97.766°
RAAN
219.8263°
Arg. of periapsis
91.2286°
True anomaly
268.89326°
Mean anomaly
268.9472°
Eccentric anomaly
268.92023°
Mean motion
3.73306 °/min
Orbital period
96.44 mins
BSTAR
0.00032568
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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 | 2026-09-20 20:33:13.628Z | 123.302° SE | 2026-09-20 20:36:13.628Z | 62.961° ENE | 29.069° | 2026-09-20 20:39:13.628Z | 12.54° NNE |
| 4 mins | 2026-09-20 22:10:13.628Z | 240.388° WSW | 2026-09-20 22:11:13.628Z | 259.899° W | 21.047° | 2026-09-20 22:14:13.628Z | 311.224° NW |
| 6 mins | 2026-09-21 09:52:13.628Z | 27.764° NE | 2026-09-21 09:54:13.628Z | 72.975° E | 55.897° | 2026-09-21 09:58:13.628Z | 179.35° S |
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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