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 52493U 26145.47130192 +.00000000 +00000-0 +45846-3 0 00001
2 52493 53.2126 64.4339 0001360 97.2754 262.8393 15.08799571 02
| Epoch (UTC): | 25 May 2026 11:18:40 |
| Eccentricity: | 0.0001360 |
| inclination: | 53.2126° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 64.4339° |
| argument of perigee: | 97.2754° |
| revolutions per day: | 15.08799571 |
| mean anomaly at epoch: | 262.8393° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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