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 32218U 99025CVQ 22225.87672182 .00001485 00000-0 46999-3 0 9993
2 32218 98.7254 358.9682 0083144 120.3850 32.7414 14.39679079787090
| Epoch (UTC): | 13 August 2022 21:02:28 |
| Eccentricity: | 0.0083144 |
| inclination: | 98.7254° |
| perigee height: | 700 km |
| apogee height: | 819 km |
| right ascension of ascending node: | 358.9682° |
| argument of perigee: | 120.3850° |
| revolutions per day: | 14.39679079 |
| mean anomaly at epoch: | 32.7414° |
| orbit number at epoch: | 78709 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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