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 25940U 99057A 24276.81131070 .00001589 00000-0 55787-3 0 9990
2 25940 98.8177 258.7480 0005785 43.7018 316.4624 14.36435116308140
| Epoch (UTC): | 02 October 2024 19:28:17 |
| Eccentricity: | 0.0005785 |
| inclination: | 98.8177° |
| perigee height: | 766 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 258.7480° |
| argument of perigee: | 43.7018° |
| revolutions per day: | 14.36435116 |
| mean anomaly at epoch: | 316.4624° |
| orbit number at epoch: | 30814 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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