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, 7.0 m
Radar Cross Section
0.080 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 ACS 3
1 59588U 24077B 26310.95958943 .00027777 00000-0 18398-1 0 9999
2 59588 97.2764 199.0677 0086477 9.6983 350.5831 13.99530294127974Epoch: 2026-11-06T23:01Z
TLE epoch observation values (Epoch: 2026-11-06T23:01:48.526Z)
Latitude
-0.00003°
Longitude
167.4438°
Altitude
836.301 km
Speed
7.466 km/s
True Right ascension
13h 16m 16s
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
03:32:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
955.42 km
Perigee altitude
829.671 km
Semi-major axis
7,270.682 km
Eccentricity
0.00865
Inclination
97.2764°
RAAN
199.0677°
Arg. of periapsis
9.6983°
True anomaly
350.41922°
Mean anomaly
350.5831°
Eccentric anomaly
350.50133°
Mean motion
3.50091 °/min
Orbital period
102.83 mins
BSTAR
0.018398
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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 | 2026-11-07 16:18:15.129Z | 148.115° SSE | 2026-11-07 16:23:15.129Z | 58.062° ENE | 54.133° | 2026-11-07 16:28:15.129Z | 357.437° N |
| 5 mins | 2026-11-07 18:03:15.129Z | 246.104° WSW | 2026-11-07 18:05:15.129Z | 272.65° WNW | 17.906° | 2026-11-07 18:08:15.129Z | 308.213° NW |
| 9 mins | 2026-11-08 04:48:15.129Z | 37.143° NE | 2026-11-08 04:52:15.129Z | 101.776° ESE | 39.174° | 2026-11-08 04:57:15.129Z | 162.759° S |
| 8 mins | 2026-11-08 06:30:15.129Z | 339.597° N | 2026-11-08 06:33:15.129Z | 298.536° NW | 30.353° | 2026-11-08 06:38:15.129Z | 235.405° WSW |
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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