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 13086U 26150.58949205 +.00000000 +00000-0 +00000-0 0 00007
2 13086 9.3257 309.3844 0003234 316.5284 356.5571 0.98192239 03
| Epoch (UTC): | 30 May 2026 14:08:52 |
| Eccentricity: | 0.0003234 |
| inclination: | 9.3257° |
| perigee height: | 36366 km |
| apogee height: | 36394 km |
| right ascension of ascending node: | 309.3844° |
| argument of perigee: | 316.5284° |
| revolutions per day: | 0.98192239 |
| mean anomaly at epoch: | 356.5571° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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