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 35935U 09051E 25191.60805043 .00000486 00000-0 11233-3 0 9995
2 35935 98.4295 88.2348 0006732 209.8258 150.2559 14.59593127838898
| Epoch (UTC): | 10 July 2025 14:35:35 |
| Eccentricity: | 0.0006732 |
| inclination: | 98.4295° |
| perigee height: | 690 km |
| apogee height: | 699 km |
| right ascension of ascending node: | 88.2348° |
| argument of perigee: | 209.8258° |
| revolutions per day: | 14.59593127 |
| mean anomaly at epoch: | 150.2559° |
| orbit number at epoch: | 83889 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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