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 00350U 26108.22680397 +.00000000 +00000-0 +11282-3 0 00002
2 00350 66.9139 23.7688 0126309 197.2643 162.4140 14.22615827 07
| Epoch (UTC): | 18 April 2026 05:26:35 |
| Eccentricity: | 0.0126309 |
| inclination: | 66.9139° |
| perigee height: | 726 km |
| apogee height: | 907 km |
| right ascension of ascending node: | 23.7688° |
| argument of perigee: | 197.2643° |
| revolutions per day: | 14.22615827 |
| mean anomaly at epoch: | 162.4140° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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