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 19460U 26088.21877667 +.00000000 +00000-0 +63977-4 0 00007
2 19460 84.9900 159.5623 0003688 37.5046 322.6404 14.34421741 05
| Epoch (UTC): | 29 March 2026 05:15:02 |
| Eccentricity: | 0.0003688 |
| inclination: | 84.9900° |
| perigee height: | 774 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 159.5623° |
| argument of perigee: | 37.5046° |
| revolutions per day: | 14.34421741 |
| mean anomaly at epoch: | 322.6404° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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