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 19649U 88102A 22181.35807118 .00000175 00000-0 11558-3 0 9991
2 19649 70.9984 165.4254 0004359 18.2236 341.9042 14.14763687734417
| Epoch (UTC): | 30 June 2022 08:35:37 |
| Eccentricity: | 0.0004359 |
| inclination: | 70.9984° |
| perigee height: | 840 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 165.4254° |
| argument of perigee: | 18.2236° |
| revolutions per day: | 14.14763687 |
| mean anomaly at epoch: | 341.9042° |
| orbit number at epoch: | 73441 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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