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 22179.63835141 .00000038 00000-0 32700-4 0 9997
2 22825 98.8857 210.9122 0008879 26.3549 333.8083 14.30177368499756
| Epoch (UTC): | 28 June 2022 15:19:13 |
| Eccentricity: | 0.0008879 |
| inclination: | 98.8857° |
| perigee height: | 785 km |
| apogee height: | 797 km |
| right ascension of ascending node: | 210.9122° |
| argument of perigee: | 26.3549° |
| revolutions per day: | 14.30177368 |
| mean anomaly at epoch: | 333.8083° |
| orbit number at epoch: | 49975 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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