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 23227U 26105.64992564 +.00000000 +00000-0 +00000-0 0 00008
2 23227 12.2635 30.8022 0006625 1.4422 14.2970 0.98697885 07
| Epoch (UTC): | 15 April 2026 15:35:53 |
| Eccentricity: | 0.0006625 |
| inclination: | 12.2635° |
| perigee height: | 36205 km |
| apogee height: | 36262 km |
| right ascension of ascending node: | 30.8022° |
| argument of perigee: | 1.4422° |
| revolutions per day: | 0.98697885 |
| mean anomaly at epoch: | 14.2970° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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