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 26097.13772455 +.00000000 +00000-0 +46111-4 0 00005
2 14453 81.1624 109.8481 0104896 116.7171 244.4792 14.25446616 05
| Epoch (UTC): | 07 April 2026 03:18:19 |
| Eccentricity: | 0.0104896 |
| inclination: | 81.1624° |
| perigee height: | 732 km |
| apogee height: | 882 km |
| right ascension of ascending node: | 109.8481° |
| argument of perigee: | 116.7171° |
| revolutions per day: | 14.25446616 |
| mean anomaly at epoch: | 244.4792° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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