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 23087.07883726 .00000024 00000-0 10000-3 0 9998
2 32953 82.5094 7.5424 0020131 4.1628 355.9617 12.43121050673575
| Epoch (UTC): | 28 March 2023 01:53:31 |
| Eccentricity: | 0.0020131 |
| inclination: | 82.5094° |
| perigee height: | 1477 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 7.5424° |
| argument of perigee: | 4.1628° |
| revolutions per day: | 12.43121050 |
| mean anomaly at epoch: | 355.9617° |
| orbit number at epoch: | 67357 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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