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 35350U 01049QJ 22175.72389075 .00000758 00000-0 20875-3 0 9993
2 35350 98.6045 173.6635 0073877 135.5592 225.1561 14.48297500473043
| Epoch (UTC): | 24 June 2022 17:22:24 |
| Eccentricity: | 0.0073877 |
| inclination: | 98.6045° |
| perigee height: | 678 km |
| apogee height: | 784 km |
| right ascension of ascending node: | 173.6635° |
| argument of perigee: | 135.5592° |
| revolutions per day: | 14.48297500 |
| mean anomaly at epoch: | 225.1561° |
| orbit number at epoch: | 47304 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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