View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 37224U 26075.02872169 +.00000000 +00000-0 +23869-3 0 00007
2 37224 71.9702 291.2934 0016673 245.9620 113.9806 14.93315452 02
| Epoch (UTC): | 16 March 2026 00:41:21 |
| Eccentricity: | 0.0016673 |
| inclination: | 71.9702° |
| perigee height: | 576 km |
| apogee height: | 599 km |
| right ascension of ascending node: | 291.2934° |
| argument of perigee: | 245.9620° |
| revolutions per day: | 14.93315452 |
| mean anomaly at epoch: | 113.9806° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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