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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 LEMUR 2 DELOITTE-1
1 63259U 25052BB 26206.26612687 .00003566 00000-0 30810-3 0 9998
2 63259 97.6888 98.4362 0002302 47.9122 312.2295 14.97847474 74399Epoch: 2026-07-25T06:23Z
TLE epoch observation values (Epoch: 2026-07-25T06:23:13.361Z)
Latitude
-0.0001°
Longitude
59.64967°
Altitude
575.525 km
Speed
7.574 km/s
True Right ascension
06h 33m 44s
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
19:21:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
572.156 km
Perigee altitude
568.957 km
Semi-major axis
6,948.693 km
Eccentricity
0.00023
Inclination
97.6888°
RAAN
98.4362°
Arg. of periapsis
47.9122°
True anomaly
312.20996°
Mean anomaly
312.2295°
Eccentric anomaly
312.21973°
Mean motion
3.74704 °/min
Orbital period
96.08 mins
BSTAR
0.0003081
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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 | 2026-07-26 16:13:14.005Z | 106.159° ESE | 2026-07-26 16:14:14.005Z | 83.503° E | 24.866° | 2026-07-26 16:17:14.005Z | 19.493° NNE |
| 4 mins | 2026-07-26 17:48:14.005Z | 233.567° WSW | 2026-07-26 17:50:14.005Z | 272.69° WNW | 19.203° | 2026-07-26 17:52:14.005Z | 306.949° NW |
| 6 mins | 2026-07-27 05:28:14.005Z | 32.027° NE | 2026-07-27 05:30:14.005Z | 89.566° E | 38.798° | 2026-07-27 05:34:14.005Z | 177.805° S |
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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