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 26073.62276856 +.00000000 +00000-0 +51907-4 0 00006
2 14453 81.1658 133.5395 0103883 184.4835 175.5426 14.25440821 04
| Epoch (UTC): | 14 March 2026 14:56:47 |
| Eccentricity: | 0.0103883 |
| inclination: | 81.1658° |
| perigee height: | 732 km |
| apogee height: | 882 km |
| right ascension of ascending node: | 133.5395° |
| argument of perigee: | 184.4835° |
| revolutions per day: | 14.25440821 |
| mean anomaly at epoch: | 175.5426° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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