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 26141.16090617 +.00000000 +00000-0 +26790-3 0 00001
2 00746 60.8785 224.9070 2991258 219.9223 113.8749 9.10831339 01
| Epoch (UTC): | 21 May 2026 03:51:42 |
| Eccentricity: | 0.2991258 |
| inclination: | 60.8785° |
| perigee height: | 410 km |
| apogee height: | 6204 km |
| right ascension of ascending node: | 224.9070° |
| argument of perigee: | 219.9223° |
| revolutions per day: | 9.10831339 |
| mean anomaly at epoch: | 113.8749° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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