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 52666U 26145.47077745 +.00000000 +00000-0 +16984-4 0 00009
2 52666 53.2133 169.0491 0000945 73.5693 286.5403 15.08842465 06
| Epoch (UTC): | 25 May 2026 11:17:55 |
| Eccentricity: | 0.0000945 |
| inclination: | 53.2133° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 169.0491° |
| argument of perigee: | 73.5693° |
| revolutions per day: | 15.08842465 |
| mean anomaly at epoch: | 286.5403° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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