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 02766U 26148.52225105 +.00000000 +00000-0 +00000-0 0 00007
2 02766 36.4866 5.2796 4640335 121.7860 358.7111 0.21294873 07
| Epoch (UTC): | 28 May 2026 12:32:02 |
| Eccentricity: | 0.4640335 |
| inclination: | 36.4866° |
| perigee height: | 57110 km |
| apogee height: | 167043 km |
| right ascension of ascending node: | 5.2796° |
| argument of perigee: | 121.7860° |
| revolutions per day: | 0.21294873 |
| mean anomaly at epoch: | 358.7111° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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