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 23706U 26088.15976333 +.00000000 +00000-0 +16106-3 0 00009
2 23706 70.9991 232.1897 0198375 157.7585 14.7510 13.74415034 08
| Epoch (UTC): | 29 March 2026 03:50:03 |
| Eccentricity: | 0.0198375 |
| inclination: | 70.9991° |
| perigee height: | 838 km |
| apogee height: | 1130 km |
| right ascension of ascending node: | 232.1897° |
| argument of perigee: | 157.7585° |
| revolutions per day: | 13.74415034 |
| mean anomaly at epoch: | 14.7510° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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