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 62560U 26145.58335647 +.00000000 +00000-0 +12640-3 0 00007
2 62560 43.0012 36.8018 0001722 268.8658 8.3610 15.70806119 08
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001722 |
| inclination: | 43.0012° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 36.8018° |
| argument of perigee: | 268.8658° |
| revolutions per day: | 15.70806119 |
| mean anomaly at epoch: | 8.3610° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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