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 22627U 93024B 24281.35074916 .00001694 00000-0 22363-3 0 9998
2 22627 82.5211 140.4816 0021585 238.8251 121.0846 14.79362083696505
| Epoch (UTC): | 07 October 2024 08:25:04 |
| Eccentricity: | 0.0021585 |
| inclination: | 82.5211° |
| perigee height: | 616 km |
| apogee height: | 646 km |
| right ascension of ascending node: | 140.4816° |
| argument of perigee: | 238.8251° |
| revolutions per day: | 14.79362083 |
| mean anomaly at epoch: | 121.0846° |
| orbit number at epoch: | 69650 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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