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 26159.08500119 +.00000000 +00000-0 +68745-4 0 00009
2 23343 97.6994 186.1848 0005181 291.9630 131.0433 14.79494909 03
| Epoch (UTC): | 08 June 2026 02:02:24 |
| Eccentricity: | 0.0005181 |
| inclination: | 97.6994° |
| perigee height: | 627 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 186.1848° |
| argument of perigee: | 291.9630° |
| revolutions per day: | 14.79494909 |
| mean anomaly at epoch: | 131.0433° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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