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 52356U 26145.45013064 +.00000000 +00000-0 +51303-4 0 00001
2 52356 53.2126 214.5583 0000988 86.0764 274.0341 15.08838917 07
| Epoch (UTC): | 25 May 2026 10:48:11 |
| Eccentricity: | 0.0000988 |
| inclination: | 53.2126° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 214.5583° |
| argument of perigee: | 86.0764° |
| revolutions per day: | 15.08838917 |
| mean anomaly at epoch: | 274.0341° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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