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TOMORROW-S2, 60485

Orbit data source: Space-Track

TOMORROW-S2, 60485 is a payload satellite owned by Tomorrow.io (US) in SSO that was launched on Fri, 16 Aug 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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<iframe src="https://www.satcat.com/sats-embedded/60485?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/60485?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

60485, 2024-149T

Orbit

SSO

Country

US

Related business

Tomorrow.io (The Tomorrow Companies Inc.) (US)

Manufacturer

Blue Canyon

Mission

Operational Commercial Weather

Bus & Motor

CUBESAT 6U, Unknown motor

Mass

12 kg wet, 12 kg dry

Launch date (UTC)

2024-08-16 (2 years ago)

Launch vehicle

FALCON 9

Launch site

Air Force Western Test Range (AFWTR)

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: 14 hours ago

TLE from 14 hours ago

0 TOMORROW-S2
1 60485U 24149T   26144.66166450  .00006514  00000-0  21101-3 0  9998
2 60485  97.3815 225.6814 0002940  31.6183 328.5235 15.32353690 98487

Epoch: 2026-05-24T15:52Z

TLE epoch observation values (Epoch: 2026-05-24T15:52:47.812Z)

Latitude

-0.00005°

Longitude

105.22159°

Altitude

470.183 km

Speed

7.632 km/s

True Right ascension

15h 02m 43s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow 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

14:39:53

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

467.752 km

Perigee altitude

463.728 km

Semi-major axis

6,843.877 km

Eccentricity

0.00029

Inclination

97.3815°

RAAN

225.6814°

Arg. of periapsis

31.6183°

True anomaly

328.5059°

Mean anomaly

328.5235°

Eccentric anomaly

328.5147°

Mean motion

3.83345 °/min

Orbital period

93.91 mins

BSTAR

0.00021101

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Other satellites on launch #149 in the year 2024 (2024-08-16 UTC)

OBJECT AU, 60510

FLOCK 4BE 16, 60483 (Decayed)

PICO-02C023, 60564 (Decayed)

FLOCK 4BE 32, 60497

SATORO-T2, 60477 (Decayed)

FLOCK 4BE 19, 60563

FLOCK 4BE 33, 60502 (Decayed)

OBJECT BP, 60529 (Decayed)

FLOCK 4BE 9, 60514

HAWK-10A, 60540

LEMU-NGE, 60532

Did you know?

You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.

Click here to try in Sandbox

TOMORROW-S2 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	2026-05-25 06:07:05.523Z	215.497° SW	2026-05-25 06:09:05.523Z	258.733° W	22.208°	2026-05-25 06:12:05.523Z	319.703° NNW

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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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Check out TOMORROW-S2, 60485 on other resources

View TOMORROW-S2, 60485 on NASA - NSSDCA Website

View TOMORROW-S2, 60485 on Heavens-Above

View TOMORROW-S2, 60485 on Keep Track

View TOMORROW-S2, 60485 on Celestrak

View TOMORROW-S2, 60485 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

Documentation

Go to standalone docs website

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