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 25338U 98030A 22136.14650278 .00000214 00000-0 10773-3 0 9996
2 25338 98.6467 166.1004 0011000 37.8540 322.3412 14.26123501248668
| Epoch (UTC): | 16 May 2022 03:30:57 |
| Eccentricity: | 0.0011000 |
| inclination: | 98.6467° |
| perigee height: | 797 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 166.1004° |
| argument of perigee: | 37.8540° |
| revolutions per day: | 14.26123501 |
| mean anomaly at epoch: | 322.3412° |
| orbit number at epoch: | 24866 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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