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 40920U 15050A 23331.92849406 .00000015 00000-0 37003-4 0 9993
2 40920 82.4897 300.0294 0008322 217.7819 142.2677 12.42878661371042
| Epoch (UTC): | 27 November 2023 22:17:01 |
| Eccentricity: | 0.0008322 |
| inclination: | 82.4897° |
| perigee height: | 1488 km |
| apogee height: | 1501 km |
| right ascension of ascending node: | 300.0294° |
| argument of perigee: | 217.7819° |
| revolutions per day: | 12.42878661 |
| mean anomaly at epoch: | 142.2677° |
| orbit number at epoch: | 37104 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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