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 25194.16002493 .00000022 00000-0 78937-6 0 9993
2 41917 86.3959 230.1487 0001724 87.8277 272.3116 14.34217682444611
| Epoch (UTC): | 13 July 2025 03:50:26 |
| Eccentricity: | 0.0001724 |
| inclination: | 86.3959° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 230.1487° |
| argument of perigee: | 87.8277° |
| revolutions per day: | 14.34217682 |
| mean anomaly at epoch: | 272.3116° |
| orbit number at epoch: | 44461 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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