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 26575U 26140.54842845 +.00000000 +00000-0 +00000-0 0 00001
2 26575 11.5789 35.6517 0003059 33.1835 141.1601 1.00276027 04
| Epoch (UTC): | 20 May 2026 13:09:44 |
| Eccentricity: | 0.0003059 |
| inclination: | 11.5789° |
| perigee height: | 35773 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 35.6517° |
| argument of perigee: | 33.1835° |
| revolutions per day: | 1.00276027 |
| mean anomaly at epoch: | 141.1601° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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