REAL, 64875
Orbit data source: Space-Track
REAL, 64875 is a payload satellite owned by Dartmouth (US) in SSO that was launched on Wed, 23 Jul 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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64875 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Dartmouth
Mission
Operational Amateur Science
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
5 kg wet, 5 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 REAL
1 64875U 25154G 26270.12776555 .00020518 00000-0 57219-3 0 9995
2 64875 97.3931 338.7769 0001533 113.6025 246.5381 15.36787447 65683Epoch: 2026-09-27T03:03Z
TLE epoch observation values (Epoch: 2026-09-27T03:03:58.943Z)
Latitude
0.00004°
Longitude
-73.14463°
Altitude
459.147 km
Speed
7.637 km/s
True Right ascension
22h 35m 06s
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
21:48:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
453.607 km
Perigee altitude
451.512 km
Semi-major axis
6,830.696 km
Eccentricity
0.00015
Inclination
97.3931°
RAAN
338.7769°
Arg. of periapsis
113.6025°
True anomaly
246.52199°
Mean anomaly
246.5381°
Eccentric anomaly
246.53004°
Mean motion
3.84455 °/min
Orbital period
93.64 mins
BSTAR
0.00057219
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Other satellites on launch #154 in the year 2025 (2025-07-23 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.REAL 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 | 2026-09-28 17:08:49.466Z | 40.24° NE | 2026-09-28 17:10:49.466Z | 97.662° ESE | 36.412° | 2026-09-28 17:13:49.466Z | 165.901° 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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