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SENTINEL 1A, 39634

Orbit data source: Space-Track

SENTINEL 1A, 39634 is a payload satellite owned by ESA (ESA) in SSO that was launched on Thu, 03 Apr 2014 UTC via a SOYUZ-ST-A launch vehicle from the French Guiana (FRGUI). 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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https://www.satcat.com/sats-embedded/39634?theme=dark&initialShowStats=false

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Identifier

39634, 2014-016A

Orbit

SSO

Country

ESA

Related business

European Space Agency (FR)

Manufacturer

Thales Alenia

Mission

Operational Civil Radar Imaging

Bus & Motor

PRIMA, AOCS

Mass

2,157 kg wet, 2,027 kg dry

Launch date (UTC)

2014-04-03 (13 years ago)

Launch vehicle

SOYUZ-ST-A

Launch site

French Guiana (FRGUI)

Object type

Payload

Rocket body

Debris

Shape & HBR

Box + 4 Pan, 10.5 m

Radar Cross Section

19.705 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 6 hours ago

TLE from 6 hours ago

0 SENTINEL 1A
1 39634U 14016A   26275.86640644 -.00000034  00000-0  24946-5 0  9995
2 39634  98.1599 281.7076 0001476  84.4601 275.6767 14.59809138665724

Epoch: 2026-10-02T20:47Z

TLE epoch observation values (Epoch: 2026-10-02T20:47:37.516Z)

Latitude

-0.00006°

Longitude

-41.78092°

Altitude

696.673 km

Speed

7.508 km/s

True Right ascension

18h 46m 49s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

Unknown

Longitude

Unknown

Altitude

Unknown

Speed

Unknown

Apparent Right ascension

Unknown

Apparent Declination

Unknown

Sunlit

N/A

Visualization observer readout

Local Sidereal Time

20:41:31

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

691.913 km

Perigee altitude

689.827 km

Semi-major axis

7,069.007 km

Eccentricity

0.00015

Inclination

98.1599°

RAAN

281.7076°

Arg. of periapsis

84.4601°

True anomaly

275.65987°

Mean anomaly

275.6767°

Eccentric anomaly

275.66828°

Mean motion

3.65179 °/min

Orbital period

98.58 mins

BSTAR

0.0000024946

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Other satellites on launch #16 in the year 2014 (2014-04-03 UTC)

SENTINEL 1A DEB, 41800 (Decayed)

SENTINEL 1A DEB, 41801 (Decayed)

SENTINEL 1A DEB, 41802 (Decayed)

SENTINEL 1A DEB, 41804 (Decayed)

SENTINEL 1A DEB, 41798 (Decayed)

SENTINEL 1A DEB, 43417 (Decayed)

SENTINEL 1A DEB, 41799 (Decayed)

SENTINEL 1A DEB, 41803 (Decayed)

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SENTINEL 1A 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.
4 mins	2026-10-03 12:12:39.506Z	63.134° ENE	2026-10-03 12:14:39.506Z	91° ESE	15.754°	2026-10-03 12:16:39.506Z	119.284° SE
7 mins	2026-10-03 13:49:39.506Z	354.282° N	2026-10-03 13:52:39.506Z	282.686° WNW	50.32°	2026-10-03 13:56:39.506Z	214.3° SW
4 mins	2026-10-03 23:17:39.506Z	86.801° E	2026-10-03 23:19:39.506Z	56.837° ENE	16.435°	2026-10-03 23:21:39.506Z	30.093° NE
7 mins	2026-10-04 00:53:39.506Z	193.154° SSW	2026-10-04 00:56:39.506Z	275.771° WNW	50.691°	2026-10-04 01:00:39.506Z	335.946° NNW

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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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Check out SENTINEL 1A, 39634 on other resources

View SENTINEL 1A, 39634 on NASA - NSSDCA Website

View SENTINEL 1A, 39634 on Heavens-Above

View SENTINEL 1A, 39634 on Keep Track

View SENTINEL 1A, 39634 on Celestrak

View SENTINEL 1A, 39634 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

SENTINEL 1A, 39634

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 6 hours ago

TLE from 6 hours ago

TLE epoch observation values (Epoch: 2026-10-02T20:47:37.516Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #16 in the year 2014 (2014-04-03 UTC)

SENTINEL 1A Visibility forecast

Co-orbital & Co-planar RSOs

Check out SENTINEL 1A, 39634 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 6 hours ago