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 54190C 22141AK 23084.72340278 .00041534 00000-0 26082-2 0 841
2 54190 53.2156 162.3975 0001281 86.6514 69.6085 15.08744894 13
| Epoch (UTC): | 25 March 2023 17:21:42 |
| Eccentricity: | 0.0001281 |
| inclination: | 53.2156° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 162.3975° |
| argument of perigee: | 86.6514° |
| revolutions per day: | 15.08744894 |
| mean anomaly at epoch: | 69.6085° |
| orbit number at epoch: | 1 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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