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 69123U 26144.65318426 +.00000000 +00000-0 -42379-3 0 00005
2 69123 70.0007 229.2745 0009123 259.5159 100.4951 14.57062785 04
| Epoch (UTC): | 24 May 2026 15:40:35 |
| Eccentricity: | 0.0009123 |
| inclination: | 70.0007° |
| perigee height: | 696 km |
| apogee height: | 709 km |
| right ascension of ascending node: | 229.2745° |
| argument of perigee: | 259.5159° |
| revolutions per day: | 14.57062785 |
| mean anomaly at epoch: | 100.4951° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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