HORACIO, 59098
Orbit data source: Space-Track
HORACIO, 59098 is a payload satellite owned by Satlantis (ES) in SSO that was launched on Mon, 04 Mar 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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59098 intel report (Beta)
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Identifier
Orbit
Country
ES / SPNRelated business
Manufacturer
NanoAvionics
Mission
Operational Commercial Imaging
Bus & Motor
CUBESAT 16U M16P, Unknown motor
Mass
~20 kg wet, ~20 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.100 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 HORACIO
1 59098U 24043A 26286.92746703 .00003044 00000-0 25648-3 0 9995
2 59098 97.8701 59.6184 0009975 357.2432 2.8734 14.98939392142451Epoch: 2026-10-13T22:15Z
TLE epoch observation values (Epoch: 2026-10-13T22:15:33.151Z)
Latitude
0.00001°
Longitude
63.24575°
Altitude
566.296 km
Speed
7.582 km/s
True Right ascension
03h 58m 28s
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
23:25:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
574.114 km
Perigee altitude
560.258 km
Semi-major axis
6,945.323 km
Eccentricity
0.001
Inclination
97.8701°
RAAN
59.6184°
Arg. of periapsis
357.2432°
True anomaly
2.87914°
Mean anomaly
2.8734°
Eccentric anomaly
2.87627°
Mean motion
3.74977 °/min
Orbital period
96.01 mins
BSTAR
0.00025648
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Other satellites on launch #43 in the year 2024 (2024-03-04 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.HORACIO 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 | 2026-10-14 08:01:52.457Z | 103.287° ESE | 2026-10-14 08:03:52.457Z | 68.683° E | 18.814° | 2026-10-14 08:05:52.457Z | 33.178° NE |
| 5 mins | 2026-10-14 09:36:52.457Z | 215.295° SW | 2026-10-14 09:38:52.457Z | 264.38° W | 31.946° | 2026-10-14 09:41:52.457Z | 322.585° NNW |
| 5 mins | 2026-10-14 21:16:52.457Z | 48.876° ENE | 2026-10-14 21:18:52.457Z | 95.664° ESE | 32.089° | 2026-10-14 21:21:52.457Z | 156.011° SSE |
| 4 mins | 2026-10-14 22:51:52.457Z | 326.844° NNW | 2026-10-14 22:53:52.457Z | 291.22° WNW | 19.362° | 2026-10-14 22:55:52.457Z | 256.535° 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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