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 65749U 26145.49849499 +.00000000 +00000-0 +20722-3 0 00004
2 65749 53.1587 336.1019 0000408 126.3833 233.7206 15.30195284 04
| Epoch (UTC): | 25 May 2026 11:57:49 |
| Eccentricity: | 0.0000408 |
| inclination: | 53.1587° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 336.1019° |
| argument of perigee: | 126.3833° |
| revolutions per day: | 15.30195284 |
| mean anomaly at epoch: | 233.7206° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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