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 14453U 26070.32364160 +.00000000 +00000-0 +54058-4 0 00006
2 14453 81.1665 136.8626 0103710 194.0452 165.7840 14.25439944 01
| Epoch (UTC): | 11 March 2026 07:46:02 |
| Eccentricity: | 0.0103710 |
| inclination: | 81.1665° |
| perigee height: | 732 km |
| apogee height: | 882 km |
| right ascension of ascending node: | 136.8626° |
| argument of perigee: | 194.0452° |
| revolutions per day: | 14.25439944 |
| mean anomaly at epoch: | 165.7840° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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