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 23342U 26106.29071753 +.00000000 +00000-0 +53569-4 0 00008
2 23342 97.6674 127.1121 0000966 85.0336 275.0989 14.85008408 04
| Epoch (UTC): | 16 April 2026 06:58:37 |
| Eccentricity: | 0.0000966 |
| inclination: | 97.6674° |
| perigee height: | 613 km |
| apogee height: | 614 km |
| right ascension of ascending node: | 127.1121° |
| argument of perigee: | 85.0336° |
| revolutions per day: | 14.85008408 |
| mean anomaly at epoch: | 275.0989° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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