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 54171U 22141Q 23084.53049768 -.00008059 00000-0 -48927-3 0 9994
2 54171 53.2164 177.8895 0001436 62.2029 297.9109 15.08806157 22722
| Epoch (UTC): | 25 March 2023 12:43:55 |
| Eccentricity: | 0.0001436 |
| inclination: | 53.2164° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 177.8895° |
| argument of perigee: | 62.2029° |
| revolutions per day: | 15.08806157 |
| mean anomaly at epoch: | 297.9109° |
| orbit number at epoch: | 2272 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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