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 62052U 26145.55575541 +.00000000 +00000-0 -10972-3 0 00006
2 62052 42.9994 188.9410 0001804 272.2219 87.8426 15.27552076 08
| Epoch (UTC): | 25 May 2026 13:20:17 |
| Eccentricity: | 0.0001804 |
| inclination: | 42.9994° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 188.9410° |
| argument of perigee: | 272.2219° |
| revolutions per day: | 15.27552076 |
| mean anomaly at epoch: | 87.8426° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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