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 52685U 26145.43494367 +.00000000 +00000-0 +63771-4 0 00005
2 52685 53.2135 159.5971 0001119 75.5016 284.6101 15.08844086 06
| Epoch (UTC): | 25 May 2026 10:26:19 |
| Eccentricity: | 0.0001119 |
| inclination: | 53.2135° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 159.5971° |
| argument of perigee: | 75.5016° |
| revolutions per day: | 15.08844086 |
| mean anomaly at epoch: | 284.6101° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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