Showing default

TOMORROW-S4, 62386

Orbit data source: Space-Track

TOMORROW-S4, 62386 is a payload satellite owned by Tomorrow.io (US) in LEO that was launched on Sat, 21 Dec 2024 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.

Loading next visibility...
Identifier
62386, 2024-247K
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)
2024-12-21 (8 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 0.6 m
Radar Cross Section
0.138 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 TOMORROW-S4
1 62386U 24247K   25240.96737613  .00007790  00000-0  33040-3 0  9995
2 62386  44.9914  86.3716 0005532 154.9659 205.1491 15.23646149 38298
Epoch: 2025-08-28T23:13Z
TLE epoch observation values (Epoch: 2025-08-28T23:13:01.297Z)
Latitude
-0.00006°
Longitude
120.69335°
Altitude
498.293 km
Speed
7.615 km/s
True Right ascension
05h 45m 29s
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
16:56:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
500.265 km
Perigee altitude
492.659 km
Semi-major axis
6,874.599 km
Eccentricity
0.00055
Inclination
44.9914°
RAAN
86.3716°
Arg. of periapsis
154.9659°
True anomaly
205.12218°
Mean anomaly
205.1491°
Eccentric anomaly
205.13564°
Mean motion
3.80778 °/min
Orbital period
94.54 mins
BSTAR
0.0003304
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
|