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 23148.04111111 .00010250 00000-0 18588-3 0 9999
2 25544 51.6411 68.4016 0005324 29.4351 150.7933 15.50217990398662
| Epoch (UTC): | 28 May 2023 00:59:12 |
| Eccentricity: | 0.0005324 |
| inclination: | 51.6411° |
| perigee height: | 412 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 68.4016° |
| argument of perigee: | 29.4351° |
| revolutions per day: | 15.50217990 |
| mean anomaly at epoch: | 150.7933° |
| orbit number at epoch: | 39866 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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