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 00746U 26109.10454764 +.00000000 +00000-0 +61327-3 0 00001
2 00746 60.8786 268.3476 2989860 211.7489 126.2649 9.10733852 02
| Epoch (UTC): | 19 April 2026 02:30:32 |
| Eccentricity: | 0.2989860 |
| inclination: | 60.8786° |
| perigee height: | 412 km |
| apogee height: | 6204 km |
| right ascension of ascending node: | 268.3476° |
| argument of perigee: | 211.7489° |
| revolutions per day: | 9.10733852 |
| mean anomaly at epoch: | 126.2649° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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