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 26140.14195830 +.00000000 +00000-0 +00000-0 0 00004
2 23435 14.4970 355.2735 0007632 296.2061 239.5264 0.99079955 02
| Epoch (UTC): | 20 May 2026 03:24:25 |
| Eccentricity: | 0.0007632 |
| inclination: | 14.4970° |
| perigee height: | 36092 km |
| apogee height: | 36156 km |
| right ascension of ascending node: | 355.2735° |
| argument of perigee: | 296.2061° |
| revolutions per day: | 0.99079955 |
| mean anomaly at epoch: | 239.5264° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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