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 11869U 26100.14755610 +.00000000 +00000-0 +46025-4 0 00007
2 11869 74.0461 160.6011 0013228 14.5070 345.6459 14.34635825 04
| Epoch (UTC): | 10 April 2026 03:32:28 |
| Eccentricity: | 0.0013228 |
| inclination: | 74.0461° |
| perigee height: | 767 km |
| apogee height: | 786 km |
| right ascension of ascending node: | 160.6011° |
| argument of perigee: | 14.5070° |
| revolutions per day: | 14.34635825 |
| mean anomaly at epoch: | 345.6459° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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