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 14154U 26099.88462105 +.00000000 +00000-0 +15212-3 0 00002
2 14154 82.0251 224.5131 0040374 136.7190 344.2898 14.38669956 03
| Epoch (UTC): | 09 April 2026 21:13:51 |
| Eccentricity: | 0.0040374 |
| inclination: | 82.0251° |
| perigee height: | 734 km |
| apogee height: | 792 km |
| right ascension of ascending node: | 224.5131° |
| argument of perigee: | 136.7190° |
| revolutions per day: | 14.38669956 |
| mean anomaly at epoch: | 344.2898° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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