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 26554U 26145.54727937 +.00000000 +00000-0 +00000-0 0 00007
2 26554 2.0704 81.6460 0003055 334.3190 200.1811 1.00272004 07
| Epoch (UTC): | 25 May 2026 13:08:04 |
| Eccentricity: | 0.0003055 |
| inclination: | 2.0704° |
| perigee height: | 35774 km |
| apogee height: | 35799 km |
| right ascension of ascending node: | 81.6460° |
| argument of perigee: | 334.3190° |
| revolutions per day: | 1.00272004 |
| mean anomaly at epoch: | 200.1811° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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