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 22136.56746214 .00000228 00000-0 11355-3 0 9990
2 25338 98.6466 166.5160 0010975 36.7434 323.4497 14.26123833248476
| Epoch (UTC): | 16 May 2022 13:37:08 |
| Eccentricity: | 0.0010975 |
| inclination: | 98.6466° |
| perigee height: | 797 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 166.5160° |
| argument of perigee: | 36.7434° |
| revolutions per day: | 14.26123833 |
| mean anomaly at epoch: | 323.4497° |
| orbit number at epoch: | 24847 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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