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 25510U 98061C 23271.13309541 .00003489 00000-0 58673-3 0 9994
2 25510 31.4361 293.2288 0320683 279.7042 76.7509 14.39381515307677
| Epoch (UTC): | 28 September 2023 03:11:39 |
| Eccentricity: | 0.0320683 |
| inclination: | 31.4361° |
| perigee height: | 531 km |
| apogee height: | 989 km |
| right ascension of ascending node: | 293.2288° |
| argument of perigee: | 279.7042° |
| revolutions per day: | 14.39381515 |
| mean anomaly at epoch: | 76.7509° |
| orbit number at epoch: | 30767 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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