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 52585U 26145.23299522 +.00000000 +00000-0 +96709-4 0 00005
2 52585 53.2122 135.4660 0001150 80.2373 279.8749 15.08848453 09
| Epoch (UTC): | 25 May 2026 05:35:30 |
| Eccentricity: | 0.0001150 |
| inclination: | 53.2122° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 135.4660° |
| argument of perigee: | 80.2373° |
| revolutions per day: | 15.08848453 |
| mean anomaly at epoch: | 279.8749° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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