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 11060U 78096A 25073.55519275 .00000432 00000-0 22635-3 0 9994
2 11060 98.4993 109.4304 0011465 130.3841 229.8338 14.19128372613553
| Epoch (UTC): | 14 March 2025 13:19:28 |
| Eccentricity: | 0.0011465 |
| inclination: | 98.4993° |
| perigee height: | 820 km |
| apogee height: | 836 km |
| right ascension of ascending node: | 109.4304° |
| argument of perigee: | 130.3841° |
| revolutions per day: | 14.19128372 |
| mean anomaly at epoch: | 229.8338° |
| orbit number at epoch: | 61355 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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