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 24340.57529992 .00001179 00000-0 26512-3 0 9990
2 27561 98.5125 178.5402 0045721 53.9630 306.5791 14.57774264169267
| Epoch (UTC): | 05 December 2024 13:48:25 |
| Eccentricity: | 0.0045721 |
| inclination: | 98.5125° |
| perigee height: | 668 km |
| apogee height: | 733 km |
| right ascension of ascending node: | 178.5402° |
| argument of perigee: | 53.9630° |
| revolutions per day: | 14.57774264 |
| mean anomaly at epoch: | 306.5791° |
| orbit number at epoch: | 16926 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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