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 52660U 26145.45979903 +.00000000 +00000-0 +11013-4 0 00006
2 52660 53.2108 169.4853 0000686 114.2298 245.8766 15.08835665 08
| Epoch (UTC): | 25 May 2026 11:02:06 |
| Eccentricity: | 0.0000686 |
| inclination: | 53.2108° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 169.4853° |
| argument of perigee: | 114.2298° |
| revolutions per day: | 15.08835665 |
| mean anomaly at epoch: | 245.8766° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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