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 10114U 77057B 25118.88330375 .00013248 00000-0 35784-3 0 9995
2 10114 97.5486 274.6851 0007780 344.3167 15.7835 15.37854769619843
| Epoch (UTC): | 28 April 2025 21:11:57 |
| Eccentricity: | 0.0007780 |
| inclination: | 97.5486° |
| perigee height: | 447 km |
| apogee height: | 458 km |
| right ascension of ascending node: | 274.6851° |
| argument of perigee: | 344.3167° |
| revolutions per day: | 15.37854769 |
| mean anomaly at epoch: | 15.7835° |
| orbit number at epoch: | 61984 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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