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 22135.84273216 .00000708 00000-0 17215-3 0 9990
2 35935 98.5770 352.5811 0008428 155.2875 204.8727 14.55950788671133
| Epoch (UTC): | 15 May 2022 20:13:32 |
| Eccentricity: | 0.0008428 |
| inclination: | 98.5770° |
| perigee height: | 700 km |
| apogee height: | 712 km |
| right ascension of ascending node: | 352.5811° |
| argument of perigee: | 155.2875° |
| revolutions per day: | 14.55950788 |
| mean anomaly at epoch: | 204.8727° |
| orbit number at epoch: | 67113 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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