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 35938U 09052B 23076.16065828 0.00000020 00000-0 94078-4 0 05
2 35938 57.9856 119.2459 0022287 124.1839 235.9657 12.74804660 05
| Epoch (UTC): | 17 March 2023 03:51:20 |
| Eccentricity: | 0.0022287 |
| inclination: | 57.9856° |
| perigee height: | 1345 km |
| apogee height: | 1379 km |
| right ascension of ascending node: | 119.2459° |
| argument of perigee: | 124.1839° |
| revolutions per day: | 12.74804660 |
| mean anomaly at epoch: | 235.9657° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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