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 65718U 26145.45127983 +.00000000 +00000-0 +19288-3 0 00008
2 65718 49.9918 51.4102 0009825 149.8004 210.3502 14.83043522 07
| Epoch (UTC): | 25 May 2026 10:49:50 |
| Eccentricity: | 0.0009825 |
| inclination: | 49.9918° |
| perigee height: | 613 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 51.4102° |
| argument of perigee: | 149.8004° |
| revolutions per day: | 14.83043522 |
| mean anomaly at epoch: | 210.3502° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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