LEMUR 2 HUBBLE-5, 64840
Orbit data source: Space-Track
LEMUR 2 HUBBLE-5, 64840 is an American payload satellite in SSO that was launched on Mon, 23 Jun 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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64840 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 16U, Unknown motor
Mass
22 kg wet, 22 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 4 Pan, 1.4 m
Radar Cross Section
0.326 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 LEMUR 2 HUBBLE-5
1 64840U 25135BT 26224.27521510 .00000863 00000-0 85667-4 0 9990
2 64840 97.7758 338.2448 0006563 140.9212 219.2484 14.94284157 62281Epoch: 2026-08-12T06:36Z
TLE epoch observation values (Epoch: 2026-08-12T06:36:18.584Z)
Latitude
0.00004°
Longitude
-81.56413°
Altitude
591.181 km
Speed
7.563 km/s
True Right ascension
22h 32m 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
17:40:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
586.179 km
Perigee altitude
577.044 km
Semi-major axis
6,959.749 km
Eccentricity
0.00066
Inclination
97.7758°
RAAN
338.2448°
Arg. of periapsis
140.9212°
True anomaly
219.20085°
Mean anomaly
219.2484°
Eccentric anomaly
219.22462°
Mean motion
3.73812 °/min
Orbital period
96.31 mins
BSTAR
0.000085667
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Other satellites on launch #135 in the year 2025 (2025-06-23 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 HUBBLE-5 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 | 2026-08-13 06:51:37.770Z | 115.741° SE | 2026-08-13 06:54:37.770Z | 60.129° ENE | 21.607° | 2026-08-13 06:56:37.770Z | 24.777° NE |
| 5 mins | 2026-08-13 08:27:37.770Z | 223.766° SW | 2026-08-13 08:29:37.770Z | 266.318° W | 23.625° | 2026-08-13 08:32:37.770Z | 318.424° NNW |
| 5 mins | 2026-08-13 20:09:37.770Z | 39.573° NE | 2026-08-13 20:11:37.770Z | 94.592° ESE | 34.752° | 2026-08-13 20:14:37.770Z | 166.286° 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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