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 23087.80317317 .00000024 00000-0 10000-3 0 9997
2 32953 82.5096 7.0921 0020085 2.6561 357.4627 12.43121101673666
| Epoch (UTC): | 28 March 2023 19:16:34 |
| Eccentricity: | 0.0020085 |
| inclination: | 82.5096° |
| perigee height: | 1477 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 7.0921° |
| argument of perigee: | 2.6561° |
| revolutions per day: | 12.43121101 |
| mean anomaly at epoch: | 357.4627° |
| orbit number at epoch: | 67366 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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