ACS 3, 59588
Orbit data source: Space-Track
ACS 3, 59588 is a payload satellite owned by ARC (US) in SSO that was launched on Tue, 23 Apr 2024 UTC via an ELECTRON launch vehicle from the Rocket Lab Launch Complex (RLLC). 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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59588 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
ARC/NANAVU
Mission
Operational Civil Technology
Bus & Motor
CUBESAT 12U, Unknown motor
Mass
16.1 kg wet, 16.1 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Sail, 6.3 m
Radar Cross Section
0.080 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 ACS 3
1 59588U 24077B 26118.42628241 .00000948 00000-0 75623-3 0 9999
2 59588 97.1803 48.3648 0058343 343.7079 16.2209 13.91927163101110Epoch: 2026-04-28T10:13Z
TLE epoch observation values (Epoch: 2026-04-28T10:13:50.800Z)
Latitude
-0.00004°
Longitude
38.50137°
Altitude
883.922 km
Speed
7.431 km/s
True Right ascension
03h 13m 27s
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
22:32:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
961.589 km
Perigee altitude
876.441 km
Semi-major axis
7,297.152 km
Eccentricity
0.00583
Inclination
97.1803°
RAAN
48.3648°
Arg. of periapsis
343.7079°
True anomaly
16.40897°
Mean anomaly
16.2209°
Eccentric anomaly
16.3148°
Mean motion
3.48187 °/min
Orbital period
103.39 mins
BSTAR
0.00075623
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Other satellites on launch #77 in the year 2024 (2024-04-23 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.ACS 3 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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-04-29 19:07:10.264Z | 158.723° S | 2026-04-29 19:12:10.264Z | 75.278° E | 43.839° | 2026-04-29 19:17:10.264Z | 353.133° N |
| 10 mins | 2026-04-30 07:41:10.264Z | 24.915° NE | 2026-04-30 07:45:10.264Z | 82.682° E | 39.517° | 2026-04-30 07:51:10.264Z | 175.879° S |
| 7 mins | 2026-04-30 09:24:10.264Z | 334.441° NNW | 2026-04-30 09:27:10.264Z | 299.041° NW | 20.816° | 2026-04-30 09:31:10.264Z | 252.165° W |
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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