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 42826U 26150.42759985 +.00000000 +00000-0 +47944-3 0 00009
2 42826 97.4423 318.5448 0008154 137.7227 222.4634 15.13833000 00
| Epoch (UTC): | 30 May 2026 10:15:44 |
| Eccentricity: | 0.0008154 |
| inclination: | 97.4423° |
| perigee height: | 519 km |
| apogee height: | 530 km |
| right ascension of ascending node: | 318.5448° |
| argument of perigee: | 137.7227° |
| revolutions per day: | 15.13833000 |
| mean anomaly at epoch: | 222.4634° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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