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 68660U 26144.63244503 +.00000000 +00000-0 -56957-3 0 00009
2 68660 86.4926 51.8114 0005583 147.0687 213.0802 13.35080239 07
| Epoch (UTC): | 24 May 2026 15:10:43 |
| Eccentricity: | 0.0005583 |
| inclination: | 86.4926° |
| perigee height: | 1123 km |
| apogee height: | 1132 km |
| right ascension of ascending node: | 51.8114° |
| argument of perigee: | 147.0687° |
| revolutions per day: | 13.35080239 |
| mean anomaly at epoch: | 213.0802° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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