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 65717U 26145.14271105 +.00000000 +00000-0 +20007-3 0 00000
2 65717 49.9809 55.1142 0012555 122.4133 237.8022 14.83277065 06
| Epoch (UTC): | 25 May 2026 03:25:30 |
| Eccentricity: | 0.0012555 |
| inclination: | 49.9809° |
| perigee height: | 610 km |
| apogee height: | 628 km |
| right ascension of ascending node: | 55.1142° |
| argument of perigee: | 122.4133° |
| revolutions per day: | 14.83277065 |
| mean anomaly at epoch: | 237.8022° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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