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 23463U 26106.28406918 +.00000000 +00000-0 +76846-5 0 00000
2 23463 82.9269 61.6971 0037920 313.0930 209.5252 13.72729767 02
| Epoch (UTC): | 16 April 2026 06:49:03 |
| Eccentricity: | 0.0037920 |
| inclination: | 82.9269° |
| perigee height: | 962 km |
| apogee height: | 1018 km |
| right ascension of ascending node: | 61.6971° |
| argument of perigee: | 313.0930° |
| revolutions per day: | 13.72729767 |
| mean anomaly at epoch: | 209.5252° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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