BUGSAT 1, 40014
Orbit data source: Space-Track
BUGSAT 1, 40014 is a payload satellite owned by Satellogic SA (AR) in SSO that was launched on Thu, 19 Jun 2014 UTC via a DNEPR launch vehicle from the Orenburg, Russia (OREN). 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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40014 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / ARGNRelated business
Manufacturer
Satellogic SA
Mission
Operational Commercial Imaging
Bus & Motor
BUGSAT, Unknown motor
Mass
22 kg wet, 22 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 1.0 m
Radar Cross Section
0.263 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 BUGSAT 1
1 40014U 14033E 25299.23220559 .00007233 00000-0 41606-3 0 9990
2 40014 98.0603 13.4699 0028867 257.7848 102.0148 15.12448053620435Epoch: 2025-10-26T05:34Z
TLE epoch observation values (Epoch: 2025-10-26T05:34:22.562Z)
Latitude
-0.00002°
Longitude
-104.97546°
Altitude
536.004 km
Speed
7.592 km/s
True Right ascension
00h 53m 52s
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
09:43:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
545.671 km
Perigee altitude
505.812 km
Semi-major axis
6,903.879 km
Eccentricity
0.00289
Inclination
98.0603°
RAAN
13.4699°
Arg. of periapsis
257.7848°
True anomaly
102.3381°
Mean anomaly
102.0148°
Eccentric anomaly
102.17647°
Mean motion
3.78358 °/min
Orbital period
95.15 mins
BSTAR
0.00041606
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Other satellites on launch #33 in the year 2014 (2014-06-19 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.BUGSAT 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-26 17:15:49.552Z | 42.728° NE | 2025-10-26 17:18:49.552Z | 99.323° ESE | 22.919° | 2025-10-26 17:21:49.552Z | 152.328° SSE |
| 5 mins | 2025-10-27 05:31:49.552Z | 202.799° SW | 2025-10-27 05:33:49.552Z | 259.87° W | 33.479° | 2025-10-27 05:36:49.552Z | 328.05° NNW |
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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