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 40071U 14037C 22179.81556633 .00000586 00000-0 81464-4 0 9991
2 40071 98.4084 49.1189 0007164 284.6160 75.4253 14.81885078431020
| Epoch (UTC): | 28 June 2022 19:34:24 |
| Eccentricity: | 0.0007164 |
| inclination: | 98.4084° |
| perigee height: | 618 km |
| apogee height: | 628 km |
| right ascension of ascending node: | 49.1189° |
| argument of perigee: | 284.6160° |
| revolutions per day: | 14.81885078 |
| mean anomaly at epoch: | 75.4253° |
| orbit number at epoch: | 43102 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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