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: 16 hours ago
TLE from 16 hours ago
0 NANOACE
1 42844U 17042V 26048.46054068 .00014606 00000-0 65307-3 0 9990
2 42844 97.3644 224.9403 0005167 78.6204 281.5613 15.21403078469856Epoch: 2026-02-17T11:03Z
TLE epoch observation values (Epoch: 2026-02-17T11:03:10.714Z)
Latitude
0.00004°
Longitude
-88.29456°
Altitude
503.99 km
Speed
7.613 km/s
True Right ascension
14h 59m 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
06:15:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
502.123 km
Perigee altitude
495.017 km
Semi-major axis
6,876.707 km
Eccentricity
0.00052
Inclination
97.3644°
RAAN
224.9403°
Arg. of periapsis
78.6204°
True anomaly
281.50328°
Mean anomaly
281.5613°
Eccentric anomaly
281.53229°
Mean motion
3.80603 °/min
Orbital period
94.59 mins
BSTAR
0.00065307
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-02-18 10:53:12.451Z | 107.284° ESE | 2026-02-18 10:55:12.451Z | 67.025° ENE | 18.754° | 2026-02-18 10:57:12.451Z | 28.625° NE |
| 4 mins | 2026-02-18 12:27:12.451Z | 228.287° WSW | 2026-02-18 12:29:12.451Z | 276.484° WNW | 21.316° | 2026-02-18 12:31:12.451Z | 313.899° NW |
| 4 mins | 2026-02-18 23:57:12.451Z | 61.676° ENE | 2026-02-18 23:58:12.451Z | 88.329° E | 25.087° | 2026-02-19 00:01:12.451Z | 153.607° SSE |
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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