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 42793U 17036AE 23268.64721571 .00047888 00000-0 10396-2 0 9992
2 42793 97.1406 301.3280 0008354 100.6151 259.6039 15.44191223348376
| Epoch (UTC): | 25 September 2023 15:31:59 |
| Eccentricity: | 0.0008354 |
| inclination: | 97.1406° |
| perigee height: | 428 km |
| apogee height: | 439 km |
| right ascension of ascending node: | 301.3280° |
| argument of perigee: | 100.6151° |
| revolutions per day: | 15.44191223 |
| mean anomaly at epoch: | 259.6039° |
| orbit number at epoch: | 34837 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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