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 26088.22313140 +.00000000 +00000-0 +49336-4 0 00009
2 14453 81.1630 118.8306 0104565 142.3527 218.5032 14.25443983 04
| Epoch (UTC): | 29 March 2026 05:21:18 |
| Eccentricity: | 0.0104565 |
| inclination: | 81.1630° |
| perigee height: | 732 km |
| apogee height: | 882 km |
| right ascension of ascending node: | 118.8306° |
| argument of perigee: | 142.3527° |
| revolutions per day: | 14.25443983 |
| mean anomaly at epoch: | 218.5032° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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