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 65342U 26145.36683164 +.00000000 +00000-0 +74802-3 0 00002
2 65342 53.1592 210.0739 0000995 86.9490 273.1626 15.31713658 05
| Epoch (UTC): | 25 May 2026 08:48:14 |
| Eccentricity: | 0.0000995 |
| inclination: | 53.1592° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 210.0739° |
| argument of perigee: | 86.9490° |
| revolutions per day: | 15.31713658 |
| mean anomaly at epoch: | 273.1626° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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