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 52106U 26145.29096600 +.00000000 +00000-0 +17917-4 0 00006
2 52106 53.2145 105.2419 0001498 59.0597 301.0543 15.08842236 00
| Epoch (UTC): | 25 May 2026 06:58:59 |
| Eccentricity: | 0.0001498 |
| inclination: | 53.2145° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 105.2419° |
| argument of perigee: | 59.0597° |
| revolutions per day: | 15.08842236 |
| mean anomaly at epoch: | 301.0543° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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