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 26072.92082675 +.00000000 +00000-0 +47823-4 0 00004
2 14453 81.1660 134.2466 0103844 186.5183 173.4654 14.25440582 04
| Epoch (UTC): | 13 March 2026 22:05:59 |
| Eccentricity: | 0.0103844 |
| inclination: | 81.1660° |
| perigee height: | 732 km |
| apogee height: | 882 km |
| right ascension of ascending node: | 134.2466° |
| argument of perigee: | 186.5183° |
| revolutions per day: | 14.25440582 |
| mean anomaly at epoch: | 173.4654° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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