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 40014U 14033E 22175.95692866 .00002866 00000-0 25393-3 0 9995
2 40014 98.1413 174.6674 0031372 15.9018 344.3180 14.96745907437269
| Epoch (UTC): | 24 June 2022 22:57:58 |
| Eccentricity: | 0.0031372 |
| inclination: | 98.1413° |
| perigee height: | 555 km |
| apogee height: | 599 km |
| right ascension of ascending node: | 174.6674° |
| argument of perigee: | 15.9018° |
| revolutions per day: | 14.96745907 |
| mean anomaly at epoch: | 344.3180° |
| orbit number at epoch: | 43726 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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