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 40032U 14033Y 22176.81164604 .00001598 00000-0 17163-3 0 9992
2 40032 97.9383 109.6257 0012609 33.8628 326.3392 14.89957712435382
| Epoch (UTC): | 25 June 2022 19:28:46 |
| Eccentricity: | 0.0012609 |
| inclination: | 97.9383° |
| perigee height: | 589 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 109.6257° |
| argument of perigee: | 33.8628° |
| revolutions per day: | 14.89957712 |
| mean anomaly at epoch: | 326.3392° |
| orbit number at epoch: | 43538 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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