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 26074.88626376 +.00000000 +00000-0 +45635-4 0 00002
2 14453 81.1655 132.2668 0103948 180.8273 179.2752 14.25441018 00
| Epoch (UTC): | 15 March 2026 21:16:13 |
| Eccentricity: | 0.0103948 |
| inclination: | 81.1655° |
| perigee height: | 732 km |
| apogee height: | 882 km |
| right ascension of ascending node: | 132.2668° |
| argument of perigee: | 180.8273° |
| revolutions per day: | 14.25441018 |
| mean anomaly at epoch: | 179.2752° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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