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 23715U 26149.21255366 +.00000000 +00000-0 +22269-2 0 00006
2 23715 1.4948 333.0280 8351692 329.0918 1.0357 1.02203937 04
| Epoch (UTC): | 29 May 2026 05:06:04 |
| Eccentricity: | 0.8351692 |
| inclination: | 1.4948° |
| perigee height: | 484 km |
| apogee height: | 70023 km |
| right ascension of ascending node: | 333.0280° |
| argument of perigee: | 329.0918° |
| revolutions per day: | 1.02203937 |
| mean anomaly at epoch: | 1.0357° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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