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 65958U 26145.32144041 +.00000000 +00000-0 +30809-3 0 00006
2 65958 51.9007 9.2405 0000858 103.9390 256.1668 14.79939421 06
| Epoch (UTC): | 25 May 2026 07:42:52 |
| Eccentricity: | 0.0000858 |
| inclination: | 51.9007° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 9.2405° |
| argument of perigee: | 103.9390° |
| revolutions per day: | 14.79939421 |
| mean anomaly at epoch: | 256.1668° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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