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 23081.76703991 .00000024 00000-0 10000-3 0 9993
2 32953 82.5091 10.8437 0020313 15.4988 344.6712 12.43120838672910
| Epoch (UTC): | 22 March 2023 18:24:32 |
| Eccentricity: | 0.0020313 |
| inclination: | 82.5091° |
| perigee height: | 1477 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 10.8437° |
| argument of perigee: | 15.4988° |
| revolutions per day: | 12.43120838 |
| mean anomaly at epoch: | 344.6712° |
| orbit number at epoch: | 67291 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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