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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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: 8 hours ago
TLE from 8 hours ago
0 NANOACE
1 42844U 17042V 26128.24386179 .00010727 00000-0 44996-3 0 9997
2 42844 97.3732 303.1924 0005193 144.8005 215.3576 15.23653225481991Epoch: 2026-05-08T05:51Z
TLE epoch observation values (Epoch: 2026-05-08T05:51:09.658Z)
Latitude
-0.00004°
Longitude
-10.67627°
Altitude
500.841 km
Speed
7.612 km/s
True Right ascension
20h 12m 46s
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
21:55:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
495.36 km
Perigee altitude
488.225 km
Semi-major axis
6,869.929 km
Eccentricity
0.00052
Inclination
97.3732°
RAAN
303.1924°
Arg. of periapsis
144.8005°
True anomaly
215.32318°
Mean anomaly
215.3576°
Eccentric anomaly
215.34039°
Mean motion
3.81167 °/min
Orbital period
94.45 mins
BSTAR
0.00044996
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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 | 2026-05-08 23:46:10.136Z | 49.526° ENE | 2026-05-08 23:48:10.136Z | 88.503° E | 20.278° | 2026-05-08 23:51:10.136Z | 146.577° SSE |
| 5 mins | 2026-05-09 11:56:10.136Z | 186.9° SSW | 2026-05-09 11:58:10.136Z | 241.317° WSW | 39.285° | 2026-05-09 12:01:10.136Z | 336.087° 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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