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 14454U 26099.89076999 +.00000000 +00000-0 +57959-4 0 00003
2 14454 81.1601 75.1451 0095577 62.5569 326.5989 14.26390904 06
| Epoch (UTC): | 09 April 2026 21:22:42 |
| Eccentricity: | 0.0095577 |
| inclination: | 81.1601° |
| perigee height: | 735 km |
| apogee height: | 872 km |
| right ascension of ascending node: | 75.1451° |
| argument of perigee: | 62.5569° |
| revolutions per day: | 14.26390904 |
| mean anomaly at epoch: | 326.5989° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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