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 52658U 26145.46714310 +.00000000 +00000-0 +51757-4 0 00002
2 52658 53.2124 169.4530 0000944 89.5304 270.5796 15.08841911 03
| Epoch (UTC): | 25 May 2026 11:12:41 |
| Eccentricity: | 0.0000944 |
| inclination: | 53.2124° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 169.4530° |
| argument of perigee: | 89.5304° |
| revolutions per day: | 15.08841911 |
| mean anomaly at epoch: | 270.5796° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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