DEORBITSAIL, 40719
Orbit data source: Space-Track
DEORBITSAIL, 40719 is a payload satellite owned by Surrey Space Ctr (UK) in SSO that was launched on Fri, 10 Jul 2015 UTC via a PSLV-XL launch vehicle from the Sirharikota (SRI). 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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40719 intel report (Beta)
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Identifier
Orbit
Country
UKRelated business
Manufacturer
Surrey Space Ctr
Mission
Non-operational Amateur Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
7 kg wet, 7 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Sail, 3.5 m
Radar Cross Section
0.039 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 DEORBITSAIL
1 40719U 15032E 26306.87699808 .00005449 00000-0 38242-3 0 9998
2 40719 97.5710 161.1247 0013397 119.5574 240.6990 15.05496989612105Epoch: 2026-11-02T21:02Z
TLE epoch observation values (Epoch: 2026-11-02T21:02:52.634Z)
Latitude
-0°
Longitude
163.25767°
Altitude
557.599 km
Speed
7.58 km/s
True Right ascension
10h 44m 29s
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
02:14:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
556.25 km
Perigee altitude
537.695 km
Semi-major axis
6,925.11 km
Eccentricity
0.00134
Inclination
97.571°
RAAN
161.1247°
Arg. of periapsis
119.5574°
True anomaly
240.56523°
Mean anomaly
240.699°
Eccentric anomaly
240.63211°
Mean motion
3.7662 °/min
Orbital period
95.59 mins
BSTAR
0.00038242
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Other satellites on launch #32 in the year 2015 (2015-07-10 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.DEORBITSAIL Visibility forecast
Loading observer location...
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 | 2026-11-03 14:44:16.813Z | 190.969° SSW | 2026-11-03 14:46:16.813Z | 265.924° W | 57.127° | 2026-11-03 14:49:16.813Z | 336.503° NNW |
| 5 mins | 2026-11-04 03:56:16.813Z | 331.33° NNW | 2026-11-04 03:58:16.813Z | 277.203° WNW | 30.811° | 2026-11-04 04:01:16.813Z | 226.431° WSW |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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