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 25544U 98067A 23158.86946759 .00014998 00000-0 26481-3 0 9998
2 25544 51.6427 14.7242 0005390 62.1946 115.7588 15.50572363400345
| Epoch (UTC): | 07 June 2023 20:52:02 |
| Eccentricity: | 0.0005390 |
| inclination: | 51.6427° |
| perigee height: | 411 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 14.7242° |
| argument of perigee: | 62.1946° |
| revolutions per day: | 15.50572363 |
| mean anomaly at epoch: | 115.7588° |
| orbit number at epoch: | 40034 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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