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 26071.16597191 +.00000000 +00000-0 +55490-4 0 00002
2 14453 81.1663 136.0142 0103753 191.6014 168.2774 14.25440243 06
| Epoch (UTC): | 12 March 2026 03:58:59 |
| Eccentricity: | 0.0103753 |
| inclination: | 81.1663° |
| perigee height: | 732 km |
| apogee height: | 882 km |
| right ascension of ascending node: | 136.0142° |
| argument of perigee: | 191.6014° |
| revolutions per day: | 14.25440243 |
| mean anomaly at epoch: | 168.2774° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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