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 30325U 99025AAL 22222.36362960 .00000065 00000-0 63200-4 0 9999
2 30325 98.8601 255.9524 0017422 96.8915 263.4237 14.08468459798339
| Epoch (UTC): | 10 August 2022 08:43:37 |
| Eccentricity: | 0.0017422 |
| inclination: | 98.8601° |
| perigee height: | 852 km |
| apogee height: | 877 km |
| right ascension of ascending node: | 255.9524° |
| argument of perigee: | 96.8915° |
| revolutions per day: | 14.08468459 |
| mean anomaly at epoch: | 263.4237° |
| orbit number at epoch: | 79833 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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