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 26070.62936294 +.00000000 +00000-0 +82811-4 0 00008
2 23343 97.7108 101.3685 0005934 203.2077 269.9962 14.79410491 08
| Epoch (UTC): | 11 March 2026 15:06:16 |
| Eccentricity: | 0.0005934 |
| inclination: | 97.7108° |
| perigee height: | 627 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 101.3685° |
| argument of perigee: | 203.2077° |
| revolutions per day: | 14.79410491 |
| mean anomaly at epoch: | 269.9962° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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