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 42617U 26068.95576597 +.00000000 +00000-0 +53358-3 0 00005
2 42617 101.4799 115.5539 0179976 1.0069 119.4504 12.19447769 01
| Epoch (UTC): | 09 March 2026 22:56:18 |
| Eccentricity: | 0.0179976 |
| inclination: | 101.4799° |
| perigee height: | 1451 km |
| apogee height: | 1738 km |
| right ascension of ascending node: | 115.5539° |
| argument of perigee: | 1.0069° |
| revolutions per day: | 12.19447769 |
| mean anomaly at epoch: | 119.4504° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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