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 24281.11305230 .00005656 00000-0 12308-2 0 9990
2 35935 98.4548 167.0898 0007965 3.4179 356.7072 14.58355101798608
| Epoch (UTC): | 07 October 2024 02:42:47 |
| Eccentricity: | 0.0007965 |
| inclination: | 98.4548° |
| perigee height: | 693 km |
| apogee height: | 704 km |
| right ascension of ascending node: | 167.0898° |
| argument of perigee: | 3.4179° |
| revolutions per day: | 14.58355101 |
| mean anomaly at epoch: | 356.7072° |
| orbit number at epoch: | 79860 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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