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 32959U 08026B 22228.75031301 .00000094 00000-0 42421-4 0 9990
2 32959 98.9491 213.5269 0071168 108.4374 64.6373 14.41905019748189
| Epoch (UTC): | 16 August 2022 18:00:27 |
| Eccentricity: | 0.0071168 |
| inclination: | 98.9491° |
| perigee height: | 701 km |
| apogee height: | 803 km |
| right ascension of ascending node: | 213.5269° |
| argument of perigee: | 108.4374° |
| revolutions per day: | 14.41905019 |
| mean anomaly at epoch: | 64.6373° |
| orbit number at epoch: | 74818 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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