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 40074U 14037F 22277.13040958 .00002565 00000-0 30215-3 0 9992
2 40074 98.3645 163.4153 0003464 316.8513 43.2528 14.85751583446206
| Epoch (UTC): | 04 October 2022 03:07:47 |
| Eccentricity: | 0.0003464 |
| inclination: | 98.3645° |
| perigee height: | 609 km |
| apogee height: | 613 km |
| right ascension of ascending node: | 163.4153° |
| argument of perigee: | 316.8513° |
| revolutions per day: | 14.85751583 |
| mean anomaly at epoch: | 43.2528° |
| orbit number at epoch: | 44620 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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