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 26018.58142096 +.00000000 +00000-0 +28092-3 0 00004
2 14208 97.6111 21.3274 0024047 52.2434 308.0983 15.36992695 04
| Epoch (UTC): | 18 January 2026 13:57:14 |
| Eccentricity: | 0.0024047 |
| inclination: | 97.6111° |
| perigee height: | 439 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 21.3274° |
| argument of perigee: | 52.2434° |
| revolutions per day: | 15.36992695 |
| mean anomaly at epoch: | 308.0983° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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