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 52587U 26145.35170917 +.00000000 +00000-0 +25814-4 0 00005
2 52587 53.2127 134.8275 0001138 59.7796 300.3309 15.08845003 07
| Epoch (UTC): | 25 May 2026 08:26:27 |
| Eccentricity: | 0.0001138 |
| inclination: | 53.2127° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 134.8275° |
| argument of perigee: | 59.7796° |
| revolutions per day: | 15.08845003 |
| mean anomaly at epoch: | 300.3309° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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