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 53256U 26145.46714632 +.00000000 +00000-0 +11440-3 0 00008
2 53256 53.2124 209.4526 0001001 71.6424 288.4677 15.08847155 00
| Epoch (UTC): | 25 May 2026 11:12:41 |
| Eccentricity: | 0.0001001 |
| inclination: | 53.2124° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 209.4526° |
| argument of perigee: | 71.6424° |
| revolutions per day: | 15.08847155 |
| mean anomaly at epoch: | 288.4677° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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