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 26053.64927034 +.00000000 +00000-0 +22696-4 0 00001
2 23463 82.9245 100.6426 0040354 97.6063 19.4340 13.72726778 07
| Epoch (UTC): | 22 February 2026 15:34:56 |
| Eccentricity: | 0.0040354 |
| inclination: | 82.9245° |
| perigee height: | 960 km |
| apogee height: | 1020 km |
| right ascension of ascending node: | 100.6426° |
| argument of perigee: | 97.6063° |
| revolutions per day: | 13.72726778 |
| mean anomaly at epoch: | 19.4340° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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