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The NASA/German Space Agency (DLR) Gravity Recovery and Climate Experiment/GRACE Follow-on (GRACE and GRACE-FO) platform consists of two identical satellites that act in unison as the primary instrument. The two satellites comprising each mission orbit one behind the other in the same orbital plane at an approximate distance between the two satellites of 220 km (137 miles). As the satellite pair circles Earth, areas of slightly stronger gravity affect the lead satellite first, pulling it toward the planet and away from the trailing satellite. As the satellites continue along their orbital path, the trailing satellite passes over the gravity anomaly and is pulled toward the lead satellite. An extremely precise microwave ranging system aboard both GRACE and GRACE-FO detects minute changes in the distance between the satellite pairs.

Instrument Type

Altimeter

Instrument Subtype

Radar Altimeter

Specifications

Resolution

Spatial

>150,000 km2

Temporal

Monthly (with a significant time lag)

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