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 14760U 26159.48151654 +.00000000 +00000-0 +54156-4 0 00003
2 14760 74.0423 224.3783 0027723 356.2909 3.8034 14.37209888 02
| Epoch (UTC): | 08 June 2026 11:33:23 |
| Eccentricity: | 0.0027723 |
| inclination: | 74.0423° |
| perigee height: | 748 km |
| apogee height: | 788 km |
| right ascension of ascending node: | 224.3783° |
| argument of perigee: | 356.2909° |
| revolutions per day: | 14.37209888 |
| mean anomaly at epoch: | 3.8034° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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