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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 (8 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: 20 hours ago

TLE from 20 hours ago
0 TOMORROW-S7
1 63631U 25081B   25340.87730093  .00003457  00000-0  30188-3 0  9998
2 63631  45.3924 253.7874 0002593 311.3268  48.7387 14.98698874 34319
Epoch: 2025-12-06T21:03Z
TLE epoch observation values (Epoch: 2025-12-06T21:03:18.800Z)
Latitude
0.00002°
Longitude
-137.93965°
Altitude
569.769 km
Speed
7.578 km/s
True Right ascension
16h 55m 08s
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
15:16:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
574.242 km
Perigee altitude
570.637 km
Semi-major axis
6,950.576 km
Eccentricity
0.00026
Inclination
45.3924°
RAAN
253.7874°
Arg. of periapsis
311.3268°
True anomaly
48.76104°
Mean anomaly
48.7387°
Eccentric anomaly
48.74987°
Mean motion
3.74552 °/min
Orbital period
96.11 mins
BSTAR
0.00030188
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Other satellites on launch #81 in the year 2025 (2025-04-22 UTC)

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