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 26068.49197066 +.00000000 +00000-0 +34094-3 0 00005
2 14208 97.6146 73.0616 0020097 226.6725 133.2845 15.38412190 01
| Epoch (UTC): | 09 March 2026 11:48:26 |
| Eccentricity: | 0.0020097 |
| inclination: | 97.6146° |
| perigee height: | 437 km |
| apogee height: | 465 km |
| right ascension of ascending node: | 73.0616° |
| argument of perigee: | 226.6725° |
| revolutions per day: | 15.38412190 |
| mean anomaly at epoch: | 133.2845° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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