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 32954U 08025B 23083.81023135 .00000008 00000-0 -14012-4 0 9998
2 32954 82.5077 11.2051 0021378 26.2510 333.9650 12.42722144672981
| Epoch (UTC): | 24 March 2023 19:26:43 |
| Eccentricity: | 0.0021378 |
| inclination: | 82.5077° |
| perigee height: | 1478 km |
| apogee height: | 1512 km |
| right ascension of ascending node: | 11.2051° |
| argument of perigee: | 26.2510° |
| revolutions per day: | 12.42722144 |
| mean anomaly at epoch: | 333.9650° |
| orbit number at epoch: | 67298 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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