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 23335.76680495 .00000031 00000-0 15483-3 0 9996
2 32953 82.5045 212.8655 0018986 176.6940 183.4269 12.43132740704474
| Epoch (UTC): | 01 December 2023 18:24:11 |
| Eccentricity: | 0.0018986 |
| inclination: | 82.5045° |
| perigee height: | 1478 km |
| apogee height: | 1508 km |
| right ascension of ascending node: | 212.8655° |
| argument of perigee: | 176.6940° |
| revolutions per day: | 12.43132740 |
| mean anomaly at epoch: | 183.4269° |
| orbit number at epoch: | 70447 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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