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 23407U 26088.02804279 +.00000000 +00000-0 +98656-4 0 00003
2 23407 71.0344 196.7141 0199297 352.0446 188.8151 13.73777687 05
| Epoch (UTC): | 29 March 2026 00:40:22 |
| Eccentricity: | 0.0199297 |
| inclination: | 71.0344° |
| perigee height: | 839 km |
| apogee height: | 1133 km |
| right ascension of ascending node: | 196.7141° |
| argument of perigee: | 352.0446° |
| revolutions per day: | 13.73777687 |
| mean anomaly at epoch: | 188.8151° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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