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 52626U 26145.64241139 +.00000000 +00000-0 +49460-4 0 00009
2 52626 53.2137 283.6673 0001014 88.6595 271.4513 15.08836326 01
| Epoch (UTC): | 25 May 2026 15:25:04 |
| Eccentricity: | 0.0001014 |
| inclination: | 53.2137° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 283.6673° |
| argument of perigee: | 88.6595° |
| revolutions per day: | 15.08836326 |
| mean anomaly at epoch: | 271.4513° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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