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: 19 hours ago
TLE from 19 hours ago
0 ACS 3
1 59588U 24077B 26137.39856968 .00000483 00000-0 39504-3 0 9997
2 59588 97.1717 63.0800 0024488 354.8515 5.2395 13.92753301103757Epoch: 2026-05-17T09:33Z
TLE epoch observation values (Epoch: 2026-05-17T09:33:56.420Z)
Latitude
-0.00005°
Longitude
44.49317°
Altitude
904.122 km
Speed
7.409 km/s
True Right ascension
04h 12m 19s
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
13:46:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
933.989 km
Perigee altitude
898.264 km
Semi-major axis
7,294.264 km
Eccentricity
0.00245
Inclination
97.1717°
RAAN
63.08°
Arg. of periapsis
354.8515°
True anomaly
5.2652°
Mean anomaly
5.2395°
Eccentric anomaly
5.25234°
Mean motion
3.48394 °/min
Orbital period
103.33 mins
BSTAR
0.00039504
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-05-18 06:51:13.410Z | 36.627° NE | 2026-05-18 06:56:13.410Z | 99.005° ESE | 25.422° | 2026-05-18 07:00:13.410Z | 147.281° SSE |
| 9 mins | 2026-05-18 08:34:13.410Z | 349.871° N | 2026-05-18 08:38:13.410Z | 289.804° WNW | 32.981° | 2026-05-18 08:43:13.410Z | 223.743° SW |
| 9 mins | 2026-05-18 18:27:13.410Z | 138.1° SSE | 2026-05-18 18:31:13.410Z | 80.903° E | 35.261° | 2026-05-18 18:36:13.410Z | 3.923° NNE |
| 7 mins | 2026-05-18 20:11:13.410Z | 230.037° WSW | 2026-05-18 20:14:13.410Z | 271.687° WNW | 22.264° | 2026-05-18 20:18:13.410Z | 318.711° NNW |
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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