DUMMY SAT, 40073
Orbit data source: Space-Track
DUMMY SAT, 40073 is a payload satellite owned by DND DSD (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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40073 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
ComDev
Mission
Non-operational Civil Technology
Bus & Motor
Unknown
Mass
75 kg wet, 75 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.4 m
Radar Cross Section
0.800 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 DUMMY SAT
1 40073U 14037E 25301.65274166 .00000769 00000-0 10243-3 0 9992
2 40073 98.3444 236.8820 0005308 350.3170 9.7939 14.82761236611120Epoch: 2025-10-28T15:39Z
TLE epoch observation values (Epoch: 2025-10-28T15:39:56.879Z)
Latitude
-0.00001°
Longitude
-35.34215°
Altitude
619.972 km
Speed
7.551 km/s
True Right ascension
15h 47m 31s
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
05:31:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
621.393 km
Perigee altitude
613.966 km
Semi-major axis
6,995.816 km
Eccentricity
0.00053
Inclination
98.3444°
RAAN
236.882°
Arg. of periapsis
350.317°
True anomaly
9.80425°
Mean anomaly
9.7939°
Eccentric anomaly
9.79908°
Mean motion
3.70925 °/min
Orbital period
97.05 mins
BSTAR
0.00010243
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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.DUMMY SAT 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 | 2025-10-29 19:20:12.082Z | 136.603° SSE | 2025-10-29 19:23:12.082Z | 71.133° E | 34.174° | 2025-10-29 19:27:12.082Z | 1.12° NNE |
| 7 mins | 2025-10-30 08:44:12.082Z | 13.851° NNE | 2025-10-30 08:47:12.082Z | 186.47° SSW | 44.546° | 2025-10-30 08:51:12.082Z | 193.885° SSW |
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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