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 26053.69269830 +.00000000 +00000-0 +10533-3 0 00002
2 14154 82.0209 267.4680 0038228 278.0638 149.5485 14.38620692 05
| Epoch (UTC): | 22 February 2026 16:37:29 |
| Eccentricity: | 0.0038228 |
| inclination: | 82.0209° |
| perigee height: | 736 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 267.4680° |
| argument of perigee: | 278.0638° |
| revolutions per day: | 14.38620692 |
| mean anomaly at epoch: | 149.5485° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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