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 23340.57504088 .00035840 00000-0 62743-3 0 9999
2 42778 97.1334 12.3469 0005954 175.4647 184.6661 15.50510582359325
| Epoch (UTC): | 06 December 2023 13:48:03 |
| Eccentricity: | 0.0005954 |
| inclination: | 97.1334° |
| perigee height: | 411 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 12.3469° |
| argument of perigee: | 175.4647° |
| revolutions per day: | 15.50510582 |
| mean anomaly at epoch: | 184.6661° |
| orbit number at epoch: | 35932 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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