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 32953U 08025A 22026.72909536 .00000021 00000-0 80971-4 0 9992
2 32953 82.5022 272.0623 0018701 208.8888 151.1159 12.43106936620729
| Epoch (UTC): | 26 January 2022 17:29:53 |
| Eccentricity: | 0.0018701 |
| inclination: | 82.5022° |
| perigee height: | 1479 km |
| apogee height: | 1508 km |
| right ascension of ascending node: | 272.0623° |
| argument of perigee: | 208.8888° |
| revolutions per day: | 12.43106936 |
| mean anomaly at epoch: | 151.1159° |
| orbit number at epoch: | 62072 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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