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 14450U 26103.88535308 +.00000000 +00000-0 +34278-4 0 00007
2 14450 82.9297 319.4269 0042756 179.3691 191.6657 13.76535050 07
| Epoch (UTC): | 13 April 2026 21:14:54 |
| Eccentricity: | 0.0042756 |
| inclination: | 82.9297° |
| perigee height: | 945 km |
| apogee height: | 1008 km |
| right ascension of ascending node: | 319.4269° |
| argument of perigee: | 179.3691° |
| revolutions per day: | 13.76535050 |
| mean anomaly at epoch: | 191.6657° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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