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 26064U 26150.77085742 +.00000000 +00000-0 +68928-4 0 00002
2 26064 100.1898 77.1614 0037795 106.9851 253.5477 14.37265395 02
| Epoch (UTC): | 30 May 2026 18:30:02 |
| Eccentricity: | 0.0037795 |
| inclination: | 100.1898° |
| perigee height: | 741 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 77.1614° |
| argument of perigee: | 106.9851° |
| revolutions per day: | 14.37265395 |
| mean anomaly at epoch: | 253.5477° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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