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 53526U 26145.62276712 +.00000000 +00000-0 +27561-3 0 00009
2 53526 34.9943 217.5923 0009901 215.0513 144.9550 15.21457940 06
| Epoch (UTC): | 25 May 2026 14:56:47 |
| Eccentricity: | 0.0009901 |
| inclination: | 34.9943° |
| perigee height: | 495 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 217.5923° |
| argument of perigee: | 215.0513° |
| revolutions per day: | 15.21457940 |
| mean anomaly at epoch: | 144.9550° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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