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TOMORROW-S7, 63631

Orbit data source: Space-Track

TOMORROW-S7, 63631 is a payload satellite owned by Tomorrow.io (US) in LEO that was launched on Tue, 22 Apr 2025 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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Identifier
63631, 2025-081B
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
Blue Canyon
Mission
Operational Commercial Weather
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
12 kg wet, 12 kg dry
Launch date (UTC)
2025-04-22 (10 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
0.138 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago
0 TOMORROW-S7
1 63631U 25081B   26036.19612306  .00003259  00000-0  28328-3 0  9995
2 63631  45.3931 300.9461 0002579 282.8732  77.1857 14.99035094 43369
Epoch: 2026-02-05T04:42Z
TLE epoch observation values (Epoch: 2026-02-05T04:42:25.032Z)
Latitude
-0.00007°
Longitude
94.98991°
Altitude
569.521 km
Speed
7.578 km/s
True Right ascension
20h 03m 47s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
21:11:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
573.193 km
Perigee altitude
569.608 km
Semi-major axis
6,949.537 km
Eccentricity
0.00026
Inclination
45.3931°
RAAN
300.9461°
Arg. of periapsis
282.8732°
True anomaly
77.21452°
Mean anomaly
77.1857°
Eccentric anomaly
77.20011°
Mean motion
3.74636 °/min
Orbital period
96.09 mins
BSTAR
0.00028328
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Other satellites on launch #81 in the year 2025 (2025-04-22 UTC)

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