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 54033U 26145.58832178 +.00000000 +00000-0 +00000-0 0 00008
2 54033 0.0417 112.3802 0001613 7.5443 358.0402 1.00272543 06
| Epoch (UTC): | 25 May 2026 14:07:11 |
| Eccentricity: | 0.0001613 |
| inclination: | 0.0417° |
| perigee height: | 35780 km |
| apogee height: | 35793 km |
| right ascension of ascending node: | 112.3802° |
| argument of perigee: | 7.5443° |
| revolutions per day: | 1.00272543 |
| mean anomaly at epoch: | 358.0402° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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