NANOACE, 42844
Orbit data source: Space-Track
NANOACE, 42844 is a payload satellite owned by Tyvak NSS (US) in SSO that was launched on Fri, 14 Jul 2017 UTC via a SOYUZ-2-1A launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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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42844 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Tyvak NSS
Mission
Operational Commercial Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
5.2 kg wet, 5.2 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.3 m
Radar Cross Section
0.048 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 NANOACE
1 42844U 17042V 25289.11647222 .00013981 00000-0 70557-3 0 9996
2 42844 97.3627 103.6903 0005275 144.0182 216.1408 15.17212422450973Epoch: 2025-10-16T02:47Z
TLE epoch observation values (Epoch: 2025-10-16T02:47:43.199Z)
Latitude
-0.00002°
Longitude
36.87949°
Altitude
520.295 km
Speed
7.602 km/s
True Right ascension
06h 54m 45s
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
07:52:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
514.872 km
Perigee altitude
507.604 km
Semi-major axis
6,889.375 km
Eccentricity
0.00053
Inclination
97.3627°
RAAN
103.6903°
Arg. of periapsis
144.0182°
True anomaly
216.10517°
Mean anomaly
216.1408°
Eccentric anomaly
216.12298°
Mean motion
3.79554 °/min
Orbital period
94.85 mins
BSTAR
0.00070557
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Other satellites on launch #42 in the year 2017 (2017-07-14 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.NANOACE 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-16 23:56:44.599Z | 41.98° NE | 2025-10-16 23:59:44.599Z | 103.365° ESE | 23.161° | 2025-10-17 00:01:44.599Z | 144.488° SSE |
| 4 mins | 2025-10-17 01:31:44.599Z | 323.177° NNW | 2025-10-17 01:33:44.599Z | 282.277° WNW | 17.922° | 2025-10-17 01:35:44.599Z | 247.883° W |
| 5 mins | 2025-10-17 12:10:44.599Z | 202.082° SSW | 2025-10-17 12:12:44.599Z | 273.715° WNW | 35.001° | 2025-10-17 12:15:44.599Z | 333.415° 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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