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 23081.28414911 .00000024 00000-0 10000-3 0 9991
2 32953 82.5087 11.1430 0020317 16.6143 343.5599 12.43120822672859
| Epoch (UTC): | 22 March 2023 06:49:10 |
| Eccentricity: | 0.0020317 |
| inclination: | 82.5087° |
| perigee height: | 1477 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 11.1430° |
| argument of perigee: | 16.6143° |
| revolutions per day: | 12.43120822 |
| mean anomaly at epoch: | 343.5599° |
| orbit number at epoch: | 67285 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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