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 26076.09871367 +.00000000 +00000-0 +63957-4 0 00004
2 23343 97.7098 106.6163 0006357 184.5792 239.9711 14.79416632 02
| Epoch (UTC): | 17 March 2026 02:22:08 |
| Eccentricity: | 0.0006357 |
| inclination: | 97.7098° |
| perigee height: | 627 km |
| apogee height: | 636 km |
| right ascension of ascending node: | 106.6163° |
| argument of perigee: | 184.5792° |
| revolutions per day: | 14.79416632 |
| mean anomaly at epoch: | 239.9711° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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