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 00022U 59009A 21024.51258986 .00000034 00000-0 25813-4 0 9990
2 00022 50.2835 144.6835 0138840 23.4658 337.2544 14.95388197503441
| Epoch (UTC): | 24 January 2021 12:18:07 |
| Eccentricity: | 0.0138840 |
| inclination: | 50.2835° |
| perigee height: | 484 km |
| apogee height: | 678 km |
| right ascension of ascending node: | 144.6835° |
| argument of perigee: | 23.4658° |
| revolutions per day: | 14.95388197 |
| mean anomaly at epoch: | 337.2544° |
| orbit number at epoch: | 50344 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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