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 53250U 26145.55178837 +.00000000 +00000-0 +54997-4 0 00008
2 53250 53.2123 209.0738 0001144 100.4655 259.6466 15.08839019 05
| Epoch (UTC): | 25 May 2026 13:14:34 |
| Eccentricity: | 0.0001144 |
| inclination: | 53.2123° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 209.0738° |
| argument of perigee: | 100.4655° |
| revolutions per day: | 15.08839019 |
| mean anomaly at epoch: | 259.6466° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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