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 22825U 93061C 22180.54784334 .00000032 00000-0 30084-4 0 9993
2 22825 98.8856 211.8408 0008831 23.8719 336.2871 14.30177515499881
| Epoch (UTC): | 29 June 2022 13:08:53 |
| Eccentricity: | 0.0008831 |
| inclination: | 98.8856° |
| perigee height: | 785 km |
| apogee height: | 797 km |
| right ascension of ascending node: | 211.8408° |
| argument of perigee: | 23.8719° |
| revolutions per day: | 14.30177515 |
| mean anomaly at epoch: | 336.2871° |
| orbit number at epoch: | 49988 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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