IHOPSAT-TD, 44859
Orbit data source: Space-Track
IHOPSAT-TD, 44859 is a payload satellite owned by Hera Systems (US) in LEO that was launched on Wed, 11 Dec 2019 UTC via a PSLV-QL launch vehicle from the Sirharikota (SRI). 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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44859 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Hera Systems
Mission
Operational Commercial Imaging
Bus & Motor
CUBESAT 12U, Unknown motor
Mass
22 kg wet, 22 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 IHOPSAT-TD
1 44859U 19089H 26263.10873144 .00001911 00000-0 11332-3 0 9999
2 44859 36.9661 186.0663 0006178 296.7882 63.2232 15.12239735372364Epoch: 2026-09-20T02:36Z
TLE epoch observation values (Epoch: 2026-09-20T02:36:34.396Z)
Latitude
0.00001°
Longitude
147.91536°
Altitude
526.571 km
Speed
7.603 km/s
True Right ascension
12h 24m 15s
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
11:36:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
536.563 km
Perigee altitude
528.025 km
Semi-major axis
6,910.431 km
Eccentricity
0.00062
Inclination
36.9661°
RAAN
186.0663°
Arg. of periapsis
296.7882°
True anomaly
63.28643°
Mean anomaly
63.2232°
Eccentric anomaly
63.25481°
Mean motion
3.7782 °/min
Orbital period
95.28 mins
BSTAR
0.00011332
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Other satellites on launch #89 in the year 2019 (2019-12-11 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.IHOPSAT-TD 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 | 2026-09-20 21:49:28.726Z | 186.717° SSW | 2026-09-20 21:51:28.726Z | 157.022° SSE | 15.003° | 2026-09-20 21:53:28.726Z | 124.215° SE |
| 6 mins | 2026-09-20 23:29:28.726Z | 223.827° SW | 2026-09-20 23:31:28.726Z | 174.941° S | 40.113° | 2026-09-20 23:35:28.726Z | 95.7° ESE |
| 6 mins | 2026-09-21 01:09:28.726Z | 253.449° W | 2026-09-21 01:11:28.726Z | 210.606° SW | 53.406° | 2026-09-21 01:15:28.726Z | 104.284° ESE |
| 6 mins | 2026-09-21 02:49:28.726Z | 255.145° W | 2026-09-21 02:52:28.726Z | 183.993° SSW | 34.233° | 2026-09-21 02:55:28.726Z | 133.211° SE |
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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