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 26106.77854916 +.00000000 +00000-0 +75035-4 0 00004
2 14154 82.0258 218.1055 0040640 116.3789 48.8936 14.38673454 06
| Epoch (UTC): | 16 April 2026 18:41:06 |
| Eccentricity: | 0.0040640 |
| inclination: | 82.0258° |
| perigee height: | 734 km |
| apogee height: | 792 km |
| right ascension of ascending node: | 218.1055° |
| argument of perigee: | 116.3789° |
| revolutions per day: | 14.38673454 |
| mean anomaly at epoch: | 48.8936° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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