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 53889U 26145.53618308 +.00000000 +00000-0 +57254-5 0 00006
2 53889 53.2123 339.2903 0001204 96.1858 263.9272 15.08828373 00
| Epoch (UTC): | 25 May 2026 12:52:06 |
| Eccentricity: | 0.0001204 |
| inclination: | 53.2123° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 339.2903° |
| argument of perigee: | 96.1858° |
| revolutions per day: | 15.08828373 |
| mean anomaly at epoch: | 263.9272° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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