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 41917U 17003A 25198.48567324 -.00000001 00000-0 -74847-5 0 9995
2 41917 86.3957 228.3407 0001698 91.9937 268.1453 14.34217479445239
| Epoch (UTC): | 17 July 2025 11:39:22 |
| Eccentricity: | 0.0001698 |
| inclination: | 86.3957° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 228.3407° |
| argument of perigee: | 91.9937° |
| revolutions per day: | 14.34217479 |
| mean anomaly at epoch: | 268.1453° |
| orbit number at epoch: | 44523 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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