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 18421U 87088A 24281.05708403 .00053842 00000-0 13098-2 0 9996
2 18421 82.4891 143.3812 0008498 333.1707 26.9098 15.40700193 24072
| Epoch (UTC): | 07 October 2024 01:22:12 |
| Eccentricity: | 0.0008498 |
| inclination: | 82.4891° |
| perigee height: | 438 km |
| apogee height: | 450 km |
| right ascension of ascending node: | 143.3812° |
| argument of perigee: | 333.1707° |
| revolutions per day: | 15.40700193 |
| mean anomaly at epoch: | 26.9098° |
| orbit number at epoch: | 2407 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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