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 24287.51972289 .00015393 00000-0 50908-3 0 9995
2 10114 97.5248 73.0971 0009219 325.8653 34.1995 15.31402504589574
| Epoch (UTC): | 13 October 2024 12:28:24 |
| Eccentricity: | 0.0009219 |
| inclination: | 97.5248° |
| perigee height: | 465 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 73.0971° |
| argument of perigee: | 325.8653° |
| revolutions per day: | 15.31402504 |
| mean anomaly at epoch: | 34.1995° |
| orbit number at epoch: | 58957 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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