SAPPHIRE, 39088
Orbit data source: Space-Track
SAPPHIRE, 39088 is a Canadian payload satellite in SSO that was launched on Mon, 25 Feb 2013 UTC via a PSLV 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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39088 intel report (Beta)
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Identifier
Orbit
Country
CARelated business
Manufacturer
SSTLA/MDABC
Mission
Operational Civil Early Warn
Bus & Motor
SSTL-150, Unknown motor
Mass
148 kg wet, 148 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.3 m
Radar Cross Section
0.375 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 22 hours ago
TLE from 22 hours ago
0 SAPPHIRE
1 39088U 13009C 26094.47272508 .00000241 00000-0 99030-4 0 9999
2 39088 98.4241 275.6832 0012331 107.1589 253.0948 14.35220385686006Epoch: 2026-04-04T11:20Z
TLE epoch observation values (Epoch: 2026-04-04T11:20:43.446Z)
Latitude
-0.00004°
Longitude
-87.28982°
Altitude
779.854 km
Speed
7.463 km/s
True Right ascension
18h 22m 43s
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
14:59:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
780.275 km
Perigee altitude
762.643 km
Semi-major axis
7,149.596 km
Eccentricity
0.00123
Inclination
98.4241°
RAAN
275.6832°
Arg. of periapsis
107.1589°
True anomaly
252.95966°
Mean anomaly
253.0948°
Eccentric anomaly
253.02723°
Mean motion
3.59022 °/min
Orbital period
100.27 mins
BSTAR
0.00009903
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Other satellites on launch #9 in the year 2013 (2013-02-25 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.SAPPHIRE 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 | 2026-04-05 10:55:03.090Z | 112.728° SE | 2026-04-05 10:59:03.090Z | 57.203° ENE | 20.748° | 2026-04-05 11:02:03.090Z | 18.515° NNE |
| 8 mins | 2026-04-05 12:34:03.090Z | 197.916° SSW | 2026-04-05 12:37:03.090Z | 247.952° W | 33.442° | 2026-04-05 12:42:03.090Z | 331.468° NNW |
| 8 mins | 2026-04-06 00:45:03.090Z | 22.358° NNE | 2026-04-06 00:48:03.090Z | 81.117° E | 42.871° | 2026-04-06 00:53:03.090Z | 185.427° SSW |
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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