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 65917U 26145.47957948 +.00000000 +00000-0 +46907-3 0 00001
2 65917 53.1581 169.0940 0001000 85.9848 274.1267 15.30202811 07
| Epoch (UTC): | 25 May 2026 11:30:35 |
| Eccentricity: | 0.0001000 |
| inclination: | 53.1581° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 169.0940° |
| argument of perigee: | 85.9848° |
| revolutions per day: | 15.30202811 |
| mean anomaly at epoch: | 274.1267° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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