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 22138.08140414 .00000120 00000-0 64342-4 0 9992
2 22825 98.8893 168.4733 0009256 135.1853 225.0078 14.30167251494085
| Epoch (UTC): | 18 May 2022 01:57:13 |
| Eccentricity: | 0.0009256 |
| inclination: | 98.8893° |
| perigee height: | 784 km |
| apogee height: | 798 km |
| right ascension of ascending node: | 168.4733° |
| argument of perigee: | 135.1853° |
| revolutions per day: | 14.30167251 |
| mean anomaly at epoch: | 225.0078° |
| orbit number at epoch: | 49408 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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