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 23268.06826584 0.00000020 00000-0 94115-4 0 03
2 35938 57.9814 324.5291 0015888 294.0252 65.9748 12.74812743 02
| Epoch (UTC): | 25 September 2023 01:38:18 |
| Eccentricity: | 0.0015888 |
| inclination: | 57.9814° |
| perigee height: | 1350 km |
| apogee height: | 1374 km |
| right ascension of ascending node: | 324.5291° |
| argument of perigee: | 294.0252° |
| revolutions per day: | 12.74812743 |
| mean anomaly at epoch: | 65.9748° |
| 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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