Showing default

TOMORROW-S9, 66309

Orbit data source: Space-Track

TOMORROW-S9, 66309 is a payload satellite owned by Tomorrow.io (US) in LEO that was launched on Sun, 02 Nov 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.

Loading next visibility...
Identifier
66309, 2025-248S
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)
2025-11-02 (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: 8 hours ago

TLE from 8 hours ago
0 TOMORROW-S9
1 66309U 25248S   26242.82272632  .00004206  00000-0  19841-3 0  9991
2 66309  45.4032  81.4078 0002776 135.0701 225.0411 15.21068058 45876
Epoch: 2026-08-30T19:44Z
TLE epoch observation values (Epoch: 2026-08-30T19:44:43.554Z)
Latitude
0.00002°
Longitude
166.21355°
Altitude
504.011 km
Speed
7.613 km/s
True Right ascension
05h 25m 37s
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
19:44:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
506.065 km
Perigee altitude
502.244 km
Semi-major axis
6,882.292 km
Eccentricity
0.00028
Inclination
45.4032°
RAAN
81.4078°
Arg. of periapsis
135.0701°
True anomaly
225.0186°
Mean anomaly
225.0411°
Eccentric anomaly
225.02985°
Mean motion
3.8014 °/min
Orbital period
94.7 mins
BSTAR
0.00019841
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|