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 35684U 26134.13606558 +.00000000 +00000-0 +64919-4 0 00002
2 35684 98.1415 208.7784 0044598 72.7688 287.8399 14.83828147 02
| Epoch (UTC): | 14 May 2026 03:15:56 |
| Eccentricity: | 0.0044598 |
| inclination: | 98.1415° |
| perigee height: | 586 km |
| apogee height: | 648 km |
| right ascension of ascending node: | 208.7784° |
| argument of perigee: | 72.7688° |
| revolutions per day: | 14.83828147 |
| mean anomaly at epoch: | 287.8399° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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