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 00046U 60007B 23340.03122900 .00001126 00000-0 23368-3 0 9997
2 00046 66.6900 221.4582 0212108 266.3395 91.3438 14.51167503322717
| Epoch (UTC): | 06 December 2023 00:44:58 |
| Eccentricity: | 0.0212108 |
| inclination: | 66.6900° |
| perigee height: | 571 km |
| apogee height: | 872 km |
| right ascension of ascending node: | 221.4582° |
| argument of perigee: | 266.3395° |
| revolutions per day: | 14.51167503 |
| mean anomaly at epoch: | 91.3438° |
| orbit number at epoch: | 32271 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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