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 35190U 99025DNW 22255.98619114 .00004111 00000-0 10820-2 0 9998
2 35190 98.6881 316.0488 0103640 320.6026 38.7659 14.46470944414115
| Epoch (UTC): | 12 September 2022 23:40:06 |
| Eccentricity: | 0.0103640 |
| inclination: | 98.6881° |
| perigee height: | 663 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 316.0488° |
| argument of perigee: | 320.6026° |
| revolutions per day: | 14.46470944 |
| mean anomaly at epoch: | 38.7659° |
| orbit number at epoch: | 41411 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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