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 52856U 26145.40279090 +.00000000 +00000-0 -78366-4 0 00003
2 52856 53.2124 39.7880 0001401 92.3372 267.7780 15.08838463 05
| Epoch (UTC): | 25 May 2026 09:40:01 |
| Eccentricity: | 0.0001401 |
| inclination: | 53.2124° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 39.7880° |
| argument of perigee: | 92.3372° |
| revolutions per day: | 15.08838463 |
| mean anomaly at epoch: | 267.7780° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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