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 32788U 08021F 23083.46588231 .00026117 00000-0 19976-2 0 9993
2 32788 97.5586 64.9210 0004096 284.6299 75.4471 15.01875090810486
| Epoch (UTC): | 24 March 2023 11:10:52 |
| Eccentricity: | 0.0004096 |
| inclination: | 97.5586° |
| perigee height: | 558 km |
| apogee height: | 564 km |
| right ascension of ascending node: | 64.9210° |
| argument of perigee: | 284.6299° |
| revolutions per day: | 15.01875090 |
| mean anomaly at epoch: | 75.4471° |
| orbit number at epoch: | 81048 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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