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 31702U 07027B 22127.27317522 0.00003316 00000-0 50442-3 0 06
2 31702 63.3100 50.1174 0469686 23.2637 336.7942 14.19626921 03
| Epoch (UTC): | 07 May 2022 06:33:22 |
| Eccentricity: | 0.0469686 |
| inclination: | 63.3100° |
| perigee height: | 488 km |
| apogee height: | 1165 km |
| right ascension of ascending node: | 50.1174° |
| argument of perigee: | 23.2637° |
| revolutions per day: | 14.19626921 |
| mean anomaly at epoch: | 336.7942° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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