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 54793U 26145.41886410 +.00000000 +00000-0 +66073-3 0 00006
2 54793 53.2128 34.6821 0001357 107.6598 252.4543 15.08791891 01
| Epoch (UTC): | 25 May 2026 10:03:09 |
| Eccentricity: | 0.0001357 |
| inclination: | 53.2128° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 34.6821° |
| argument of perigee: | 107.6598° |
| revolutions per day: | 15.08791891 |
| mean anomaly at epoch: | 252.4543° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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