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 25280U 98020A 24277.79838389 .00057602 00000-0 13988-2 0 9994
2 25280 97.4436 111.1157 0014027 127.6423 232.6098 15.40717647454216
| Epoch (UTC): | 03 October 2024 19:09:40 |
| Eccentricity: | 0.0014027 |
| inclination: | 97.4436° |
| perigee height: | 434 km |
| apogee height: | 453 km |
| right ascension of ascending node: | 111.1157° |
| argument of perigee: | 127.6423° |
| revolutions per day: | 15.40717647 |
| mean anomaly at epoch: | 232.6098° |
| orbit number at epoch: | 45421 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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