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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 NANOACE
1 42844U 17042V 26228.98216601 .00007928 00000-0 31351-3 0 9991
2 42844 97.3785 42.3656 0004981 144.9641 215.1926 15.25730192497348Epoch: 2026-08-16T23:34Z
TLE epoch observation values (Epoch: 2026-08-16T23:34:19.143Z)
Latitude
0.00001°
Longitude
83.41495°
Altitude
494.489 km
Speed
7.616 km/s
True Right ascension
02h 49m 27s
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
13:43:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
488.97 km
Perigee altitude
482.132 km
Semi-major axis
6,863.688 km
Eccentricity
0.0005
Inclination
97.3785°
RAAN
42.3656°
Arg. of periapsis
144.9641°
True anomaly
215.15972°
Mean anomaly
215.1926°
Eccentric anomaly
215.17616°
Mean motion
3.81687 °/min
Orbital period
94.32 mins
BSTAR
0.00031351
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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 | 2026-08-17 23:45:27.591Z | 47.436° ENE | 2026-08-17 23:47:27.591Z | 84.314° E | 19.766° | 2026-08-17 23:50:27.591Z | 144.7° SSE |
| 5 mins | 2026-08-18 11:54:27.591Z | 184.278° SSW | 2026-08-18 11:56:27.591Z | 226.871° WSW | 38.739° | 2026-08-18 11:59:27.591Z | 335.991° 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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