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 19687U 26033.29714028 +.00000000 +00000-0 +00000-0 0 00001
2 19687 13.2279 337.8635 0008702 303.9007 69.6532 0.99669800 09
| Epoch (UTC): | 02 February 2026 07:07:52 |
| Eccentricity: | 0.0008702 |
| inclination: | 13.2279° |
| perigee height: | 35919 km |
| apogee height: | 35993 km |
| right ascension of ascending node: | 337.8635° |
| argument of perigee: | 303.9007° |
| revolutions per day: | 0.99669800 |
| mean anomaly at epoch: | 69.6532° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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