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 11060U 26140.29309850 +.00000000 +00000-0 +56373-4 0 00008
2 11060 98.4547 162.6083 0009626 329.6573 30.4045 14.19366094 00
| Epoch (UTC): | 20 May 2026 07:02:03 |
| Eccentricity: | 0.0009626 |
| inclination: | 98.4547° |
| perigee height: | 821 km |
| apogee height: | 834 km |
| right ascension of ascending node: | 162.6083° |
| argument of perigee: | 329.6573° |
| revolutions per day: | 14.19366094 |
| mean anomaly at epoch: | 30.4045° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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