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: 17 hours ago
TLE from 17 hours ago
0 TOMORROW-S4
1 62386U 24247K 25300.54236280 .00010577 00000-0 42900-3 0 9992
2 62386 44.9910 122.8028 0005215 141.5369 218.5885 15.24827027 47386Epoch: 2025-10-27T13:01Z
TLE epoch observation values (Epoch: 2025-10-27T13:01:00.145Z)
Latitude
-0.00006°
Longitude
-108.59057°
Altitude
494.103 km
Speed
7.618 km/s
True Right ascension
08h 11m 12s
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
01:37:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
496.497 km
Perigee altitude
489.33 km
Semi-major axis
6,871.051 km
Eccentricity
0.00052
Inclination
44.991°
RAAN
122.8028°
Arg. of periapsis
141.5369°
True anomaly
218.55125°
Mean anomaly
218.5885°
Eccentric anomaly
218.56987°
Mean motion
3.81073 °/min
Orbital period
94.47 mins
BSTAR
0.000429
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-10-28 14:21:00.092Z | 176.468° S | 2025-10-28 14:23:00.092Z | 140.756° SSE | 16.866° | 2025-10-28 14:25:00.092Z | 104.532° ESE |
| 6 mins | 2025-10-28 15:59:00.092Z | 243.662° WSW | 2025-10-28 16:02:00.092Z | 74.627° E | 43.38° | 2025-10-28 16:05:00.092Z | 67.01° ENE |
| 5 mins | 2025-10-28 17:39:00.092Z | 298.48° NW | 2025-10-28 17:41:00.092Z | 0.534° NNE | 32.138° | 2025-10-28 17:44:00.092Z | 61.688° ENE |
| 5 mins | 2025-10-28 19:18:00.092Z | 306.808° NW | 2025-10-28 19:20:00.092Z | 358.211° N | 35.072° | 2025-10-28 19:23:00.092Z | 81.561° E |
| 5 mins | 2025-10-28 20:57:00.092Z | 281.441° WNW | 2025-10-28 20:59:00.092Z | 232.446° WSW | 38.807° | 2025-10-28 21:02:00.092Z | 135.184° SSE |
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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