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 25320U 98026B 22176.74392115 .00000236 00000-0 69254-4 0 9998
2 25320 86.3995 188.8184 0004320 81.1669 279.0018 14.39448844267081
| Epoch (UTC): | 25 June 2022 17:51:14 |
| Eccentricity: | 0.0004320 |
| inclination: | 86.3995° |
| perigee height: | 757 km |
| apogee height: | 763 km |
| right ascension of ascending node: | 188.8184° |
| argument of perigee: | 81.1669° |
| revolutions per day: | 14.39448844 |
| mean anomaly at epoch: | 279.0018° |
| orbit number at epoch: | 26708 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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