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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Edit Public Description
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: 8 hours ago
TLE from 8 hours ago
0 HORACIO
1 59098U 24043A 25317.31902221 .00011443 00000-0 99446-3 0 9990
2 59098 97.8266 83.3107 0011701 29.4876 330.7003 14.97104844 92356Epoch: 2025-11-13T07:39Z
TLE epoch observation values (Epoch: 2025-11-13T07:39:23.518Z)
Latitude
-0.00007°
Longitude
-84.21586°
Altitude
571.799 km
Speed
7.579 km/s
True Right ascension
05h 33m 14s
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
12:23:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
580.995 km
Perigee altitude
564.729 km
Semi-major axis
6,950.999 km
Eccentricity
0.00117
Inclination
97.8266°
RAAN
83.3107°
Arg. of periapsis
29.4876°
True anomaly
330.6346°
Mean anomaly
330.7003°
Eccentric anomaly
330.66746°
Mean motion
3.74518 °/min
Orbital period
96.12 mins
BSTAR
0.00099446
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-11-13 21:03:36.496Z | 28.179° NE | 2025-11-13 21:06:36.496Z | 88.686° E | 36.005° | 2025-11-13 21:10:36.496Z | 173.675° S |
| 5 mins | 2025-11-14 07:52:36.496Z | 110.998° ESE | 2025-11-14 07:54:36.496Z | 64.532° ENE | 24.928° | 2025-11-14 07:57:36.496Z | 13.048° NNE |
| 5 mins | 2025-11-14 09:27:36.496Z | 227.828° WSW | 2025-11-14 09:29:36.496Z | 265.1° W | 19.513° | 2025-11-14 09:32:36.496Z | 314.362° NW |
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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