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 25168.47932038 .00001770 00000-0 18266-3 0 9996
2 37224 71.9697 185.0387 0013563 34.5772 325.6276 14.91497703 62225
| Epoch (UTC): | 17 June 2025 11:30:13 |
| Eccentricity: | 0.0013563 |
| inclination: | 71.9697° |
| perigee height: | 584 km |
| apogee height: | 603 km |
| right ascension of ascending node: | 185.0387° |
| argument of perigee: | 34.5772° |
| revolutions per day: | 14.91497703 |
| mean anomaly at epoch: | 325.6276° |
| orbit number at epoch: | 6222 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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