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 26064U 26141.23363125 +.00000000 +00000-0 +38814-4 0 00008
2 26064 100.1897 65.8803 0037608 133.5083 226.9234 14.37262050 01
| Epoch (UTC): | 21 May 2026 05:36:25 |
| Eccentricity: | 0.0037608 |
| inclination: | 100.1897° |
| perigee height: | 741 km |
| apogee height: | 794 km |
| right ascension of ascending node: | 65.8803° |
| argument of perigee: | 133.5083° |
| revolutions per day: | 14.37262050 |
| mean anomaly at epoch: | 226.9234° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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