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 26619U 26150.42341662 +.00000000 +00000-0 +15632-3 0 00009
2 26619 98.1161 107.3946 0008955 175.1314 184.9980 14.69172826 06
| Epoch (UTC): | 30 May 2026 10:09:43 |
| Eccentricity: | 0.0008955 |
| inclination: | 98.1161° |
| perigee height: | 657 km |
| apogee height: | 670 km |
| right ascension of ascending node: | 107.3946° |
| argument of perigee: | 175.1314° |
| revolutions per day: | 14.69172826 |
| mean anomaly at epoch: | 184.9980° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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