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 26064.13382876 +.00000000 +00000-0 +36753-3 0 00001
2 14208 97.6135 68.5385 0019788 243.6676 116.2536 15.38284953 02
| Epoch (UTC): | 05 March 2026 03:12:42 |
| Eccentricity: | 0.0019788 |
| inclination: | 97.6135° |
| perigee height: | 438 km |
| apogee height: | 465 km |
| right ascension of ascending node: | 68.5385° |
| argument of perigee: | 243.6676° |
| revolutions per day: | 15.38284953 |
| mean anomaly at epoch: | 116.2536° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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