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 65378U 26145.39582323 +.00000000 +00000-0 +49573-3 0 00006
2 65378 53.1589 171.5641 0000959 71.5146 288.5959 15.30207423 07
| Epoch (UTC): | 25 May 2026 09:29:59 |
| Eccentricity: | 0.0000959 |
| inclination: | 53.1589° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 171.5641° |
| argument of perigee: | 71.5146° |
| revolutions per day: | 15.30207423 |
| mean anomaly at epoch: | 288.5959° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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