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 27601U 02056E 24277.87738980 .00002335 00000-0 84407-3 0 9990
2 27601 98.2441 249.6362 0069614 277.6248 142.2613 14.33066207139352
| Epoch (UTC): | 03 October 2024 21:03:26 |
| Eccentricity: | 0.0069614 |
| inclination: | 98.2441° |
| perigee height: | 731 km |
| apogee height: | 831 km |
| right ascension of ascending node: | 249.6362° |
| argument of perigee: | 277.6248° |
| revolutions per day: | 14.33066207 |
| mean anomaly at epoch: | 142.2613° |
| orbit number at epoch: | 13935 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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