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 36420U 93036AZT 24280.45726442 .00002047 00000-0 70913-3 0 9992
2 36420 74.0397 349.7960 0018335 191.2127 180.4561 14.36201015788290
| Epoch (UTC): | 06 October 2024 10:58:27 |
| Eccentricity: | 0.0018335 |
| inclination: | 74.0397° |
| perigee height: | 758 km |
| apogee height: | 784 km |
| right ascension of ascending node: | 349.7960° |
| argument of perigee: | 191.2127° |
| revolutions per day: | 14.36201015 |
| mean anomaly at epoch: | 180.4561° |
| orbit number at epoch: | 78829 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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