LEMUR 2 DELOITTE-1, 63259
Orbit data source: Space-Track
LEMUR 2 DELOITTE-1, 63259 is an American payload satellite in SSO that was launched on Sat, 15 Mar 2025 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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63259 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, Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 LEMUR 2 DELOITTE-1
1 63259U 25052BB 26085.25036919 .00004907 00000-0 43191-3 0 9996
2 63259 97.7011 339.2713 0002779 64.1131 296.0377 14.96949935 56285Epoch: 2026-03-26T06:00Z
TLE epoch observation values (Epoch: 2026-03-26T06:00:31.898Z)
Latitude
-0.00006°
Longitude
65.43639°
Altitude
578.529 km
Speed
7.572 km/s
True Right ascension
22h 37m 05s
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
13:28:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
575.268 km
Perigee altitude
571.404 km
Semi-major axis
6,951.473 km
Eccentricity
0.00028
Inclination
97.7011°
RAAN
339.2713°
Arg. of periapsis
64.1131°
True anomaly
296.00908°
Mean anomaly
296.0377°
Eccentric anomaly
296.02339°
Mean motion
3.74479 °/min
Orbital period
96.13 mins
BSTAR
0.00043191
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Other satellites on launch #52 in the year 2025 (2025-03-15 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-1 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-03-27 15:51:57.388Z | 95.515° ESE | 2026-03-27 15:53:57.388Z | 60.862° ENE | 16.202° | 2026-03-27 15:55:57.388Z | 29.631° NE |
| 6 mins | 2026-03-27 17:25:57.388Z | 202.687° SW | 2026-03-27 17:28:57.388Z | 274.786° WNW | 30.131° | 2026-03-27 17:31:57.388Z | 327.497° NNW |
| 5 mins | 2026-03-28 05:07:57.388Z | 57.463° ENE | 2026-03-28 05:09:57.388Z | 108.339° ESE | 26.062° | 2026-03-28 05:12:57.388Z | 157.541° S |
| 4 mins | 2026-03-28 06:42:57.388Z | 323.169° NNW | 2026-03-28 06:44:57.388Z | 284.697° WNW | 18.93° | 2026-03-28 06:46:57.388Z | 251.252° W |
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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