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 52680U 26145.44595943 +.00000000 +00000-0 +12649-3 0 00000
2 52680 53.2122 159.3141 0001145 78.2840 281.8280 15.08829462 06
| Epoch (UTC): | 25 May 2026 10:42:10 |
| Eccentricity: | 0.0001145 |
| inclination: | 53.2122° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 159.3141° |
| argument of perigee: | 78.2840° |
| revolutions per day: | 15.08829462 |
| mean anomaly at epoch: | 281.8280° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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