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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Edit Public Description
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: 16 hours ago
TLE from 16 hours ago
0 LEMUR 2 DELOITTE-1
1 63259U 25052BB 25345.26258878 .00011360 00000-0 10257-2 0 9992
2 63259 97.7117 235.8795 0002861 54.0719 306.0767 14.95657247 40587Epoch: 2025-12-11T06:18Z
TLE epoch observation values (Epoch: 2025-12-11T06:18:07.670Z)
Latitude
-0.00005°
Longitude
61.12646°
Altitude
582.21 km
Speed
7.57 km/s
True Right ascension
15h 43m 31s
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
20:47:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
579.335 km
Perigee altitude
575.355 km
Semi-major axis
6,955.482 km
Eccentricity
0.00029
Inclination
97.7117°
RAAN
235.8795°
Arg. of periapsis
54.0719°
True anomaly
306.0502°
Mean anomaly
306.0767°
Eccentric anomaly
306.06345°
Mean motion
3.74156 °/min
Orbital period
96.22 mins
BSTAR
0.0010257
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-12 05:21:23.388Z | 30.58° NE | 2025-12-12 05:24:23.388Z | 97.632° ESE | 35.016° | 2025-12-12 05:27:23.388Z | 167.044° S |
| 5 mins | 2025-12-12 16:10:23.388Z | 115.477° SE | 2025-12-12 16:12:23.388Z | 75.981° E | 24.119° | 2025-12-12 16:15:23.388Z | 18.211° NNE |
| 4 mins | 2025-12-12 17:46:23.388Z | 234.191° WSW | 2025-12-12 17:48:23.388Z | 275.81° WNW | 20.388° | 2025-12-12 17:50:23.388Z | 309.736° NW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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