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 52598U 26145.46623240 +.00000000 +00000-0 +16260-4 0 00006
2 52598 53.2127 299.4568 0001303 98.7226 261.3914 15.08833710 07
| Epoch (UTC): | 25 May 2026 11:11:22 |
| Eccentricity: | 0.0001303 |
| inclination: | 53.2127° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 299.4568° |
| argument of perigee: | 98.7226° |
| revolutions per day: | 15.08833710 |
| mean anomaly at epoch: | 261.3914° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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