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 23696U 26139.61601090 +.00000000 +00000-0 +00000-0 0 00003
2 23696 11.5236 14.9106 0003793 183.4109 7.5042 0.98763477 04
| Epoch (UTC): | 19 May 2026 14:47:03 |
| Eccentricity: | 0.0003793 |
| inclination: | 11.5236° |
| perigee height: | 36199 km |
| apogee height: | 36231 km |
| right ascension of ascending node: | 14.9106° |
| argument of perigee: | 183.4109° |
| revolutions per day: | 0.98763477 |
| mean anomaly at epoch: | 7.5042° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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