DX 1, 40071
Orbit data source: Space-Track
DX 1, 40071 is a payload satellite owned by Dauria (CIS) in SSO that was launched on Tue, 08 Jul 2014 UTC via a SOYUZ-2-1B 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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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
Dauria
Mission
Operational Commercial Technology
Bus & Motor
DX-1, Unknown motor
Mass
21 kg wet, 21 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.060 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 DX 1
1 40071U 14037C 25255.95980706 .00001479 00000-0 16563-3 0 9995
2 40071 98.3476 196.7732 0008973 93.2755 266.9487 14.88505573604844Epoch: 2025-09-12T23:02Z
TLE epoch observation values (Epoch: 2025-09-12T23:02:07.33Z)
Latitude
0.00002°
Longitude
-140.95738°
Altitude
605.962 km
Speed
7.556 km/s
True Right ascension
13h 07m 05s
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
23:50:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
605.915 km
Perigee altitude
593.393 km
Semi-major axis
6,977.791 km
Eccentricity
0.0009
Inclination
98.3476°
RAAN
196.7732°
Arg. of periapsis
93.2755°
True anomaly
266.84603°
Mean anomaly
266.9487°
Eccentric anomaly
266.89736°
Mean motion
3.72363 °/min
Orbital period
96.68 mins
BSTAR
0.00016563
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Other satellites on launch #37 in the year 2014 (2014-07-08 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.DX 1 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 | 2025-09-13 09:16:24.343Z | 5.582° NNE | 2025-09-13 09:20:24.343Z | 268.201° W | 41.415° | 2025-09-13 09:23:24.343Z | 207.733° SW |
| 7 mins | 2025-09-13 20:08:24.343Z | 166.335° S | 2025-09-13 20:11:24.343Z | 323.832° NNW | 44.967° | 2025-09-13 20:15:24.343Z | 346.689° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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