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 data is extracted from the following two-line orbital elements,
1 37224U 10062C 25132.79591576 .00002924 00000-0 29884-3 0 9990
2 37224 71.9713 265.5684 0013195 112.9839 247.2724 14.91327199 56900
| Epoch (UTC): | 12 May 2025 19:06:07 |
| Eccentricity: | 0.0013195 |
| inclination: | 71.9713° |
| perigee height: | 584 km |
| apogee height: | 603 km |
| right ascension of ascending node: | 265.5684° |
| argument of perigee: | 112.9839° |
| revolutions per day: | 14.91327199 |
| mean anomaly at epoch: | 247.2724° |
| orbit number at epoch: | 5690 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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