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 23343U 26075.08334025 +.00000000 +00000-0 +71976-4 0 00007
2 23343 97.7100 105.6421 0006263 187.9612 232.1205 14.79415807 02
| Epoch (UTC): | 16 March 2026 02:00:00 |
| Eccentricity: | 0.0006263 |
| inclination: | 97.7100° |
| perigee height: | 627 km |
| apogee height: | 636 km |
| right ascension of ascending node: | 105.6421° |
| argument of perigee: | 187.9612° |
| revolutions per day: | 14.79415807 |
| mean anomaly at epoch: | 232.1205° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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