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 is defined by the following mean orbital elements,
1 19649U 26022.19816668 +.00000000 +00000-0 +21660-3 0 00007
2 19649 71.0013 311.7573 0007240 232.7344 127.3119 14.15189014 06
| Epoch (UTC): | 22 January 2026 04:45:21 |
| Eccentricity: | 0.0007240 |
| inclination: | 71.0013° |
| perigee height: | 836 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 311.7573° |
| argument of perigee: | 232.7344° |
| revolutions per day: | 14.15189014 |
| mean anomaly at epoch: | 127.3119° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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