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, 0.3 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 LEMUR-2 DELOITTE-2
1 68491U 26067CD 26228.44306626 .00003835 00000-0 38374-3 0 9997
2 68491 97.7606 185.6588 0002198 166.4867 193.6411 14.92001749 20705Epoch: 2026-08-16T10:38Z
TLE epoch observation values (Epoch: 2026-08-16T10:38:00.924Z)
Latitude
-0.00006°
Longitude
61.31544°
Altitude
596.226 km
Speed
7.561 km/s
True Right ascension
12h 22m 38s
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
17:03:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.245 km
Perigee altitude
587.182 km
Semi-major axis
6,966.85 km
Eccentricity
0.00022
Inclination
97.7606°
RAAN
185.6588°
Arg. of periapsis
166.4867°
True anomaly
193.63516°
Mean anomaly
193.6411°
Eccentric anomaly
193.63813°
Mean motion
3.7324 °/min
Orbital period
96.45 mins
BSTAR
0.00038374
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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 | 2026-08-17 09:43:57.813Z | 25.223° NE | 2026-08-17 09:47:57.813Z | 112.618° SE | 36.362° | 2026-08-17 09:50:57.813Z | 171.307° S |
| 6 mins | 2026-08-17 20:34:57.813Z | 121.838° SE | 2026-08-17 20:36:57.813Z | 84.114° E | 26.24° | 2026-08-17 20:40:57.813Z | 9.976° NNE |
| 5 mins | 2026-08-17 22:10:57.813Z | 229.19° WSW | 2026-08-17 22:12:57.813Z | 264.773° W | 19.195° | 2026-08-17 22:15:57.813Z | 312.942° 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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