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 23340.75664636 .00000019 00000-0 67362-4 0 9990
2 32953 82.5038 209.7635 0019167 165.7538 194.4086 12.43132972705098
| Epoch (UTC): | 06 December 2023 18:09:34 |
| Eccentricity: | 0.0019167 |
| inclination: | 82.5038° |
| perigee height: | 1478 km |
| apogee height: | 1508 km |
| right ascension of ascending node: | 209.7635° |
| argument of perigee: | 165.7538° |
| revolutions per day: | 12.43132972 |
| mean anomaly at epoch: | 194.4086° |
| orbit number at epoch: | 70509 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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