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 42759U 17034B 22182.59191310 .00002295 00000-0 14408-3 0 9994
2 42759 43.0171 254.7656 0009334 8.9772 132.2355 15.12003998278491
| Epoch (UTC): | 01 July 2022 14:12:21 |
| Eccentricity: | 0.0009334 |
| inclination: | 43.0171° |
| perigee height: | 523 km |
| apogee height: | 536 km |
| right ascension of ascending node: | 254.7656° |
| argument of perigee: | 8.9772° |
| revolutions per day: | 15.12003998 |
| mean anomaly at epoch: | 132.2355° |
| orbit number at epoch: | 27849 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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