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 35933U 09051C 24357.92440433 .00002513 00000-0 53387-3 0 9998
2 35933 98.4407 245.5495 0006575 102.3690 257.8246 14.59989449810156
| Epoch (UTC): | 22 December 2024 22:11:08 |
| Eccentricity: | 0.0006575 |
| inclination: | 98.4407° |
| perigee height: | 688 km |
| apogee height: | 698 km |
| right ascension of ascending node: | 245.5495° |
| argument of perigee: | 102.3690° |
| revolutions per day: | 14.59989449 |
| mean anomaly at epoch: | 257.8246° |
| orbit number at epoch: | 81015 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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