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 26106.71253698 +.00000000 +00000-0 +13975-3 0 00005
2 37224 71.9702 219.5572 0014944 191.1737 168.9104 14.93494774 09
| Epoch (UTC): | 16 April 2026 17:06:03 |
| Eccentricity: | 0.0014944 |
| inclination: | 71.9702° |
| perigee height: | 577 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 219.5572° |
| argument of perigee: | 191.1737° |
| revolutions per day: | 14.93494774 |
| mean anomaly at epoch: | 168.9104° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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