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 20508U 90017A 23331.77283588 .00000132 00000-0 12233-3 0 9992
2 20508 82.9583 42.8314 0044790 157.7306 322.9038 13.74396122692290
| Epoch (UTC): | 27 November 2023 18:32:53 |
| Eccentricity: | 0.0044790 |
| inclination: | 82.9583° |
| perigee height: | 951 km |
| apogee height: | 1017 km |
| right ascension of ascending node: | 42.8314° |
| argument of perigee: | 157.7306° |
| revolutions per day: | 13.74396122 |
| mean anomaly at epoch: | 322.9038° |
| orbit number at epoch: | 69229 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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