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 00005U 26068.58438433 +.00000000 +00000-0 +29145-3 0 00002
2 00005 34.2418 261.7067 1837370 49.3629 325.2840 10.85956452 09
| Epoch (UTC): | 09 March 2026 14:01:30 |
| Eccentricity: | 0.1837370 |
| inclination: | 34.2418° |
| perigee height: | 653 km |
| apogee height: | 3818 km |
| right ascension of ascending node: | 261.7067° |
| argument of perigee: | 49.3629° |
| revolutions per day: | 10.85956452 |
| mean anomaly at epoch: | 325.2840° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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