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: 14 hours ago
TLE from 14 hours ago
0 NANOACE
1 42844U 17042V 25340.39683192 .00022017 00000-0 10523-2 0 9996
2 42844 97.3606 153.5985 0004444 349.0627 11.0510 15.19017292458752Epoch: 2025-12-06T09:31Z
TLE epoch observation values (Epoch: 2025-12-06T09:31:26.277Z)
Latitude
-0.00008°
Longitude
-64.68614°
Altitude
508.895 km
Speed
7.611 km/s
True Right ascension
10h 14m 23s
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
22:00:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
508.834 km
Perigee altitude
502.715 km
Semi-major axis
6,883.911 km
Eccentricity
0.00044
Inclination
97.3606°
RAAN
153.5985°
Arg. of periapsis
349.0627°
True anomaly
11.06077°
Mean anomaly
11.051°
Eccentric anomaly
11.05588°
Mean motion
3.80006 °/min
Orbital period
94.74 mins
BSTAR
0.0010523
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-12-07 00:18:40.497Z | 22.114° NNE | 2025-12-07 00:21:40.497Z | 72.324° E | 37.806° | 2025-12-07 00:25:40.497Z | 178.352° S |
| 4 mins | 2025-12-07 10:58:40.497Z | 106.657° ESE | 2025-12-07 11:00:40.497Z | 63.419° ENE | 20.101° | 2025-12-07 11:02:40.497Z | 25.554° NE |
| 4 mins | 2025-12-07 12:32:40.497Z | 230.161° WSW | 2025-12-07 12:34:40.497Z | 275.744° WNW | 20.302° | 2025-12-07 12:36:40.497Z | 312.263° 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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