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 52656U 26145.33194306 +.00000000 +00000-0 +59039-4 0 00004
2 52656 53.2141 170.0672 0000828 66.8451 293.2628 15.08840591 06
| Epoch (UTC): | 25 May 2026 07:57:59 |
| Eccentricity: | 0.0000828 |
| inclination: | 53.2141° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 170.0672° |
| argument of perigee: | 66.8451° |
| revolutions per day: | 15.08840591 |
| mean anomaly at epoch: | 293.2628° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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