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 54026U 26144.98704345 +.00000000 +00000-0 +00000-0 0 00007
2 54026 0.0381 86.5318 0001911 337.4842 40.8987 1.00272659 03
| Epoch (UTC): | 24 May 2026 23:41:20 |
| Eccentricity: | 0.0001911 |
| inclination: | 0.0381° |
| perigee height: | 35778 km |
| apogee height: | 35794 km |
| right ascension of ascending node: | 86.5318° |
| argument of perigee: | 337.4842° |
| revolutions per day: | 1.00272659 |
| mean anomaly at epoch: | 40.8987° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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