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 40012U 26105.93323681 +.00000000 +00000-0 +16910-3 0 00009
2 40012 97.7798 259.7842 0043964 273.6319 85.9870 14.87880742 06
| Epoch (UTC): | 15 April 2026 22:23:51 |
| Eccentricity: | 0.0043964 |
| inclination: | 97.7798° |
| perigee height: | 574 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 259.7842° |
| argument of perigee: | 273.6319° |
| revolutions per day: | 14.87880742 |
| mean anomaly at epoch: | 85.9870° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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