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 65412U 26145.51743786 +.00000000 +00000-0 +10711-2 0 00002
2 65412 53.1586 235.0169 0000286 78.3913 281.7121 15.31722713 05
| Epoch (UTC): | 25 May 2026 12:25:06 |
| Eccentricity: | 0.0000286 |
| inclination: | 53.1586° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 235.0169° |
| argument of perigee: | 78.3913° |
| revolutions per day: | 15.31722713 |
| mean anomaly at epoch: | 281.7121° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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