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.
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62386 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Blue Canyon
Mission
Operational Commercial Weather
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
12 kg wet, 12 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
0.138 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 TOMORROW-S4
1 62386U 24247K 25346.97400419 .00010364 00000-0 40557-3 0 9996
2 62386 44.9791 230.1301 0003355 29.4655 330.6416 15.26051763 54477Epoch: 2025-12-12T23:22Z
TLE epoch observation values (Epoch: 2025-12-12T23:22:33.962Z)
Latitude
0.00002°
Longitude
157.58068°
Altitude
485.618 km
Speed
7.625 km/s
True Right ascension
15h 20m 31s
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
07:35:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
491.545 km
Perigee altitude
486.937 km
Semi-major axis
6,867.378 km
Eccentricity
0.00034
Inclination
44.9791°
RAAN
230.1301°
Arg. of periapsis
29.4655°
True anomaly
330.62274°
Mean anomaly
330.6416°
Eccentric anomaly
330.63217°
Mean motion
3.81379 °/min
Orbital period
94.39 mins
BSTAR
0.00040557
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Other satellites on launch #247 in the year 2024 (2024-12-21 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.TOMORROW-S4 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 | 2025-12-13 20:02:19.076Z | 235.501° WSW | 2025-12-13 20:04:19.076Z | 161.807° S | 44.061° | 2025-12-13 20:07:19.076Z | 69.644° E |
| 5 mins | 2025-12-13 21:41:19.076Z | 291.216° WNW | 2025-12-13 21:43:19.076Z | 345.85° N | 33.023° | 2025-12-13 21:46:19.076Z | 58.911° ENE |
| 6 mins | 2025-12-13 23:20:19.076Z | 304.824° NW | 2025-12-13 23:22:19.076Z | 348.049° N | 32.901° | 2025-12-13 23:26:19.076Z | 82.895° E |
| 6 mins | 2025-12-14 00:59:19.076Z | 286.304° WNW | 2025-12-14 01:02:19.076Z | 162.799° S | 40.129° | 2025-12-14 01:05:19.076Z | 126.228° SE |
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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