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 35935U 09051E 22178.10709091 .00000348 00000-0 90139-4 0 9998
2 35935 98.5721 35.9908 0008898 40.5002 319.6855 14.55999535677313
| Epoch (UTC): | 27 June 2022 02:34:12 |
| Eccentricity: | 0.0008898 |
| inclination: | 98.5721° |
| perigee height: | 700 km |
| apogee height: | 712 km |
| right ascension of ascending node: | 35.9908° |
| argument of perigee: | 40.5002° |
| revolutions per day: | 14.55999535 |
| mean anomaly at epoch: | 319.6855° |
| orbit number at epoch: | 67731 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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