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 20625U 90046B 23334.15033802 .00000369 00000-0 21566-3 0 9992
2 20625 70.9988 241.8820 0012763 133.1752 227.0439 14.14787204731167
| Epoch (UTC): | 30 November 2023 03:36:29 |
| Eccentricity: | 0.0012763 |
| inclination: | 70.9988° |
| perigee height: | 834 km |
| apogee height: | 852 km |
| right ascension of ascending node: | 241.8820° |
| argument of perigee: | 133.1752° |
| revolutions per day: | 14.14787204 |
| mean anomaly at epoch: | 227.0439° |
| orbit number at epoch: | 73116 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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