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SENTINEL-3A

Sentinel-3A is part of Europe's Copernicus Earth-observation program. Launched in 2016, it measures ocean and land surface temperature, sea-surface height, ocean color and vegetation properties for environmental monitoring and operational services.

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Object identity

NORAD ID
41335
COSPAR ID
2016-011A
Operator
Not listed
Country
Not listed
Launch date
Not listed

Immediate discovery

Why this satellite matters

Altimetry uses travel time: transmit a radar pulse, measure its return, correct for atmospheric and orbital effects, and infer the distance between satellite and sea surface with remarkable precision.

Understanding the mission

Science and engineering ideas

Altimetry uses travel time: transmit a radar pulse, measure its return, correct for atmospheric and orbital effects, and infer the distance between satellite and sea surface with remarkable precision.

Mission

Mission and purpose

These spacecraft use cameras, radiometers, radar, spectrometers, or other instruments to measure features of Earth. Repeated observations make comparisons across seasons and years possible.

  • Altimetry uses travel time: transmit a radar pulse, measure its return, correct for atmospheric and orbital effects, and infer the distance between satellite and sea surface with remarkable precision.

Design

Engineering

Altimetry uses travel time: transmit a radar pulse, measure its return, correct for atmospheric and orbital effects, and infer the distance between satellite and sea surface with remarkable precision.

Real orbital values

The mathematics

The current two-line element set reports approximately 14.2674 revolutions per day. Dividing 1,440 minutes by that value gives an estimated orbital period of 100.9 minutes.

Period

100.9 min

Representative speed

26,822 km/h

Representative altitude

810 km

Inclination

98.63°

These are representative calculations derived from current orbital elements, not fixed physical specifications. Altitude and speed change around an elliptical orbit, and predictions change as new orbital elements are published.

Launch record

Launch and deployment

Sentinel-3A launched on 16 February 2016 aboard a Rockot from Plesetsk Cosmodrome.

TransitSatellite does not estimate historical launch weather. Temperature, clouds, wind, holds, and scrub reasons will appear only when supported by traceable historical sources.

Orbit

LEO orbit explained

Low Earth orbit is the region closest to Earth used by most crewed spacecraft, many science missions, Earth-observation satellites, and large constellations. Objects move quickly and commonly complete an orbit in roughly 90 to 130 minutes.

LEO can provide detailed Earth views, lower communications delay, and easier access than higher orbits, but it covers less area per spacecraft and is more affected by atmospheric drag.

Live TransitSatellite experience

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Learning

Questions to explore

  • Why are repeated observations valuable?
  • How can satellites observe through clouds or darkness?

Evidence

Sources and data notes

Current identity and orbital elements come from CelesTrak’s public GP data. Calculated orbit values are derived from the current TLE and may change after catalog updates. Mission-history claims are added separately and require authoritative sources.

Catalog updated

Sep 18, 2026, 6:23 AM UTC

Story review

1970-01-01T00:00:00.000Z