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 24260.66593287 .00002946 00000-0 64826-3 0 9990
2 35935 98.4587 146.2928 0009174 60.4050 299.8062 14.58218512795594
| Epoch (UTC): | 16 September 2024 15:58:56 |
| Eccentricity: | 0.0009174 |
| inclination: | 98.4587° |
| perigee height: | 692 km |
| apogee height: | 705 km |
| right ascension of ascending node: | 146.2928° |
| argument of perigee: | 60.4050° |
| revolutions per day: | 14.58218512 |
| mean anomaly at epoch: | 299.8062° |
| orbit number at epoch: | 79559 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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