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 24340.65811685 .00002565 00000-0 55923-3 0 9998
2 35935 98.4506 227.6549 0007775 159.4544 200.6969 14.58772182807284
| Epoch (UTC): | 05 December 2024 15:47:41 |
| Eccentricity: | 0.0007775 |
| inclination: | 98.4506° |
| perigee height: | 691 km |
| apogee height: | 702 km |
| right ascension of ascending node: | 227.6549° |
| argument of perigee: | 159.4544° |
| revolutions per day: | 14.58772182 |
| mean anomaly at epoch: | 200.6969° |
| orbit number at epoch: | 80728 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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