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 42778U 17036P 23270.66898352 .00034643 00000-0 74863-3 0 9997
2 42778 97.1439 303.4043 0009332 92.7577 267.4740 15.44387006348513
| Epoch (UTC): | 27 September 2023 16:03:20 |
| Eccentricity: | 0.0009332 |
| inclination: | 97.1439° |
| perigee height: | 427 km |
| apogee height: | 439 km |
| right ascension of ascending node: | 303.4043° |
| argument of perigee: | 92.7577° |
| revolutions per day: | 15.44387006 |
| mean anomaly at epoch: | 267.4740° |
| orbit number at epoch: | 34851 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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