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 52640U 26145.38941336 +.00000000 +00000-0 +11471-4 0 00003
2 52640 53.2127 274.8259 0001363 105.3053 254.8090 15.08836578 05
| Epoch (UTC): | 25 May 2026 09:20:45 |
| Eccentricity: | 0.0001363 |
| inclination: | 53.2127° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 274.8259° |
| argument of perigee: | 105.3053° |
| revolutions per day: | 15.08836578 |
| mean anomaly at epoch: | 254.8090° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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