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 25168.16280579 .00000771 00000-0 17237-3 0 9998
2 35935 98.4323 64.4150 0006435 296.2509 63.8029 14.59563034835506
| Epoch (UTC): | 17 June 2025 03:54:26 |
| Eccentricity: | 0.0006435 |
| inclination: | 98.4323° |
| perigee height: | 690 km |
| apogee height: | 699 km |
| right ascension of ascending node: | 64.4150° |
| argument of perigee: | 296.2509° |
| revolutions per day: | 14.59563034 |
| mean anomaly at epoch: | 63.8029° |
| orbit number at epoch: | 83550 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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