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: 15 hours ago
TLE from 15 hours ago
0 LEMUR 2 DELOITTE-1
1 63259U 25052BB 26083.44556929 .00004917 00000-0 43297-3 0 9991
2 63259 97.7006 337.4942 0002713 65.9060 294.2446 14.96931525 56015Epoch: 2026-03-24T10:41Z
TLE epoch observation values (Epoch: 2026-03-24T10:41:37.186Z)
Latitude
0.00003°
Longitude
-4.83386°
Altitude
578.66 km
Speed
7.572 km/s
True Right ascension
22h 29m 58s
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
07:01:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
575.279 km
Perigee altitude
571.507 km
Semi-major axis
6,951.53 km
Eccentricity
0.00027
Inclination
97.7006°
RAAN
337.4942°
Arg. of periapsis
65.906°
True anomaly
294.21625°
Mean anomaly
294.2446°
Eccentric anomaly
294.23043°
Mean motion
3.74475 °/min
Orbital period
96.13 mins
BSTAR
0.00043297
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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 | 2026-03-25 04:55:38.129Z | 49.967° ENE | 2026-03-25 04:58:38.129Z | 106.128° ESE | 20.39° | 2026-03-25 05:00:38.129Z | 139.981° SSE |
| 5 mins | 2026-03-25 06:31:38.129Z | 327.916° NNW | 2026-03-25 06:33:38.129Z | 282.37° WNW | 23.895° | 2026-03-25 06:36:38.129Z | 233.722° WSW |
| 6 mins | 2026-03-25 17:18:38.129Z | 197.562° SSW | 2026-03-25 17:20:38.129Z | 244.057° WSW | 34.528° | 2026-03-25 17:24:38.129Z | 333.309° NNW |
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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