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 65957U 26145.34981373 +.00000000 +00000-0 +31833-3 0 00002
2 65957 51.9007 14.1323 0000911 106.8703 253.2360 14.79939981 07
| Epoch (UTC): | 25 May 2026 08:23:43 |
| Eccentricity: | 0.0000911 |
| inclination: | 51.9007° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 14.1323° |
| argument of perigee: | 106.8703° |
| revolutions per day: | 14.79939981 |
| mean anomaly at epoch: | 253.2360° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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