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 27909U 84069AB 23148.88259906 .00000102 00000-0 14993-3 0 9991
2 27909 65.0479 244.4159 0038612 8.2363 351.9327 13.91715837 26723
| Epoch (UTC): | 28 May 2023 21:10:56 |
| Eccentricity: | 0.0038612 |
| inclination: | 65.0479° |
| perigee height: | 894 km |
| apogee height: | 951 km |
| right ascension of ascending node: | 244.4159° |
| argument of perigee: | 8.2363° |
| revolutions per day: | 13.91715837 |
| mean anomaly at epoch: | 351.9327° |
| orbit number at epoch: | 2672 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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