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 14208U 26042.20812611 +.00000000 +00000-0 +37730-3 0 00006
2 14208 97.6134 45.8012 0020745 329.5503 30.4535 15.37734654 07
| Epoch (UTC): | 11 February 2026 04:59:42 |
| Eccentricity: | 0.0020745 |
| inclination: | 97.6134° |
| perigee height: | 439 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 45.8012° |
| argument of perigee: | 329.5503° |
| revolutions per day: | 15.37734654 |
| mean anomaly at epoch: | 30.4535° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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