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 11690U 26150.14941225 +.00000000 +00000-0 +00000-0 0 00002
2 11690 64.7730 49.1576 0488136 205.0762 336.4392 2.00577297 09
| Epoch (UTC): | 30 May 2026 03:35:09 |
| Eccentricity: | 0.0488136 |
| inclination: | 64.7730° |
| perigee height: | 18885 km |
| apogee height: | 21477 km |
| right ascension of ascending node: | 49.1576° |
| argument of perigee: | 205.0762° |
| revolutions per day: | 2.00577297 |
| mean anomaly at epoch: | 336.4392° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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