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 65340U 26145.42741385 +.00000000 +00000-0 +68246-3 0 00002
2 65340 53.1605 209.7357 0001006 86.8480 273.2636 15.31714810 04
| Epoch (UTC): | 25 May 2026 10:15:28 |
| Eccentricity: | 0.0001006 |
| inclination: | 53.1605° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 209.7357° |
| argument of perigee: | 86.8480° |
| revolutions per day: | 15.31714810 |
| mean anomaly at epoch: | 273.2636° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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