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 57632U 26145.37840036 +.00000000 +00000-0 -97047-4 0 00007
2 57632 43.0048 19.5683 0003608 263.3623 96.6818 15.27612013 04
| Epoch (UTC): | 25 May 2026 09:04:53 |
| Eccentricity: | 0.0003608 |
| inclination: | 43.0048° |
| perigee height: | 480 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 19.5683° |
| argument of perigee: | 263.3623° |
| revolutions per day: | 15.27612013 |
| mean anomaly at epoch: | 96.6818° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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