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 40508U 95015CU 24355.71779373 .00005716 00000-0 28357-2 0 9996
2 40508 99.0361 354.5436 0048737 228.2572 131.4430 14.16936756500744
| Epoch (UTC): | 20 December 2024 17:13:37 |
| Eccentricity: | 0.0048737 |
| inclination: | 99.0361° |
| perigee height: | 800 km |
| apogee height: | 871 km |
| right ascension of ascending node: | 354.5436° |
| argument of perigee: | 228.2572° |
| revolutions per day: | 14.16936756 |
| mean anomaly at epoch: | 131.4430° |
| orbit number at epoch: | 50074 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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