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: 16 hours ago
TLE from 16 hours ago
0 LEMUR 2 DELOITTE-1
1 63259U 25052BB 26260.23862886 .00003186 00000-0 27381-3 0 9990
2 63259 97.6765 151.5538 0002424 122.7828 237.3628 14.98131508 82479Epoch: 2026-09-17T05:43Z
TLE epoch observation values (Epoch: 2026-09-17T05:43:37.533Z)
Latitude
-0.00005°
Longitude
69.46869°
Altitude
576.632 km
Speed
7.572 km/s
True Right ascension
10h 06m 12s
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
14:40:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
571.361 km
Perigee altitude
567.992 km
Semi-major axis
6,947.814 km
Eccentricity
0.00024
Inclination
97.6765°
RAAN
151.5538°
Arg. of periapsis
122.7828°
True anomaly
237.33941°
Mean anomaly
237.3628°
Eccentric anomaly
237.35111°
Mean motion
3.74775 °/min
Orbital period
96.06 mins
BSTAR
0.00027381
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-18 04:45:18.664Z | 52.637° ENE | 2026-09-18 04:48:18.664Z | 101.86° ESE | 17.336° | 2026-09-18 04:50:18.664Z | 132.976° SE |
| 5 mins | 2026-09-18 06:21:18.664Z | 334.467° NNW | 2026-09-18 06:23:18.664Z | 282.23° WNW | 33.265° | 2026-09-18 06:26:18.664Z | 227.288° WSW |
| 6 mins | 2026-09-18 17:07:18.664Z | 182.628° SSW | 2026-09-18 17:10:18.664Z | 272.376° WNW | 59.949° | 2026-09-18 17:13:18.664Z | 337.533° N |
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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