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 65954U 26145.29576480 +.00000000 +00000-0 +29721-3 0 00005
2 65954 51.9013 1.8530 0000873 108.1297 251.9760 14.79940498 08
| Epoch (UTC): | 25 May 2026 07:05:54 |
| Eccentricity: | 0.0000873 |
| inclination: | 51.9013° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 1.8530° |
| argument of perigee: | 108.1297° |
| revolutions per day: | 14.79940498 |
| mean anomaly at epoch: | 251.9760° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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