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 26044.94111343 +.00000000 +00000-0 +31963-3 0 00005
2 14208 97.6129 48.6339 0020439 319.1637 40.8074 15.37802938 01
| Epoch (UTC): | 13 February 2026 22:35:12 |
| Eccentricity: | 0.0020439 |
| inclination: | 97.6129° |
| perigee height: | 439 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 48.6339° |
| argument of perigee: | 319.1637° |
| revolutions per day: | 15.37802938 |
| mean anomaly at epoch: | 40.8074° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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