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 27561U 02054C 23149.75083615 .00000405 00000-0 10111-3 0 9992
2 27561 98.5262 329.7773 0044880 324.1879 35.6311 14.56563059 88325
| Epoch (UTC): | 29 May 2023 18:01:12 |
| Eccentricity: | 0.0044880 |
| inclination: | 98.5262° |
| perigee height: | 672 km |
| apogee height: | 736 km |
| right ascension of ascending node: | 329.7773° |
| argument of perigee: | 324.1879° |
| revolutions per day: | 14.56563059 |
| mean anomaly at epoch: | 35.6311° |
| orbit number at epoch: | 8832 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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