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, 14.5 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 REAL
1 64875U 25154G 26149.41663394 .00029573 00000-0 96192-3 0 9991
2 64875 97.4045 217.7473 0001864 126.2712 233.8702 15.31836434 47174Epoch: 2026-05-29T09:59Z
TLE epoch observation values (Epoch: 2026-05-29T09:59:57.172Z)
Latitude
-0.00001°
Longitude
-179.18824°
Altitude
474.193 km
Speed
7.628 km/s
True Right ascension
14h 30m 59s
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
01:47:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
468.559 km
Perigee altitude
466.007 km
Semi-major axis
6,845.42 km
Eccentricity
0.00019
Inclination
97.4045°
RAAN
217.7473°
Arg. of periapsis
126.2712°
True anomaly
233.85295°
Mean anomaly
233.8702°
Eccentric anomaly
233.86157°
Mean motion
3.83215 °/min
Orbital period
93.94 mins
BSTAR
0.00096192
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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 | 2026-05-29 16:50:39.205Z | 43.458° NE | 2026-05-29 16:52:39.205Z | 86.527° E | 24.479° | 2026-05-29 16:55:39.205Z | 154.268° SSE |
| 4 mins | 2026-05-30 04:57:39.205Z | 206.246° SW | 2026-05-30 04:58:39.205Z | 239.744° WSW | 34.143° | 2026-05-30 05:01:39.205Z | 330.523° 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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