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 52476U 26145.18522941 +.00000000 +00000-0 -60590-4 0 00002
2 52476 53.2129 65.9590 0001567 73.5097 286.6067 15.08844154 07
| Epoch (UTC): | 25 May 2026 04:26:43 |
| Eccentricity: | 0.0001567 |
| inclination: | 53.2129° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 65.9590° |
| argument of perigee: | 73.5097° |
| revolutions per day: | 15.08844154 |
| mean anomaly at epoch: | 286.6067° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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