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 22138.49117360 .00000944 00000-0 12687-3 0 9998
2 40071 98.4145 5.7353 0009477 58.0449 302.1705 14.81814879424903
| Epoch (UTC): | 18 May 2022 11:47:17 |
| Eccentricity: | 0.0009477 |
| inclination: | 98.4145° |
| perigee height: | 617 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 5.7353° |
| argument of perigee: | 58.0449° |
| revolutions per day: | 14.81814879 |
| mean anomaly at epoch: | 302.1705° |
| orbit number at epoch: | 42490 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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