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 39440U 13066AA 25133.81249671 .00003339 00000-0 34275-3 0 9990
2 39440 97.8488 78.5645 0060441 268.5715 90.8578 14.89756214617457
| Epoch (UTC): | 13 May 2025 19:29:59 |
| Eccentricity: | 0.0060441 |
| inclination: | 97.8488° |
| perigee height: | 556 km |
| apogee height: | 641 km |
| right ascension of ascending node: | 78.5645° |
| argument of perigee: | 268.5715° |
| revolutions per day: | 14.89756214 |
| mean anomaly at epoch: | 90.8578° |
| orbit number at epoch: | 61745 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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