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 23435U 26146.26014928 +.00000000 +00000-0 +00000-0 0 00001
2 23435 14.4964 355.2306 0007244 298.5097 259.5999 0.99082695 04
| Epoch (UTC): | 26 May 2026 06:14:36 |
| Eccentricity: | 0.0007244 |
| inclination: | 14.4964° |
| perigee height: | 36092 km |
| apogee height: | 36154 km |
| right ascension of ascending node: | 355.2306° |
| argument of perigee: | 298.5097° |
| revolutions per day: | 0.99082695 |
| mean anomaly at epoch: | 259.5999° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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