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 23628U 26146.24696041 +.00000000 +00000-0 +00000-0 0 00005
2 23628 13.4008 15.8441 0002656 258.9011 282.3642 0.98664204 03
| Epoch (UTC): | 26 May 2026 05:55:37 |
| Eccentricity: | 0.0002656 |
| inclination: | 13.4008° |
| perigee height: | 36232 km |
| apogee height: | 36255 km |
| right ascension of ascending node: | 15.8441° |
| argument of perigee: | 258.9011° |
| revolutions per day: | 0.98664204 |
| mean anomaly at epoch: | 282.3642° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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