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 25168.50557567 .00000751 00000-0 16828-3 0 9993
2 35935 98.4322 64.7633 0006427 294.9989 65.0542 14.59563574835527
| Epoch (UTC): | 17 June 2025 12:08:01 |
| Eccentricity: | 0.0006427 |
| inclination: | 98.4322° |
| perigee height: | 690 km |
| apogee height: | 699 km |
| right ascension of ascending node: | 64.7633° |
| argument of perigee: | 294.9989° |
| revolutions per day: | 14.59563574 |
| mean anomaly at epoch: | 65.0542° |
| orbit number at epoch: | 83552 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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