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 00408U 61015EH 24280.89877598 .00001600 00000-0 16834-2 0 9993
2 00408 66.7854 144.5387 0068888 186.7062 185.0320 13.76335481220587
| Epoch (UTC): | 06 October 2024 21:34:14 |
| Eccentricity: | 0.0068888 |
| inclination: | 66.7854° |
| perigee height: | 926 km |
| apogee height: | 1027 km |
| right ascension of ascending node: | 144.5387° |
| argument of perigee: | 186.7062° |
| revolutions per day: | 13.76335481 |
| mean anomaly at epoch: | 185.0320° |
| orbit number at epoch: | 22058 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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