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 11669U 26150.46602330 +.00000000 +00000-0 +00000-0 0 00004
2 11669 6.2072 306.8524 0021336 244.6488 138.4792 1.00164825 02
| Epoch (UTC): | 30 May 2026 11:11:04 |
| Eccentricity: | 0.0021336 |
| inclination: | 6.2072° |
| perigee height: | 35727 km |
| apogee height: | 35907 km |
| right ascension of ascending node: | 306.8524° |
| argument of perigee: | 244.6488° |
| revolutions per day: | 1.00164825 |
| mean anomaly at epoch: | 138.4792° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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