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 65721U 26145.47180022 +.00000000 +00000-0 +19538-3 0 00005
2 65721 49.9859 53.5876 0008341 120.9109 239.2650 14.83281787 05
| Epoch (UTC): | 25 May 2026 11:19:23 |
| Eccentricity: | 0.0008341 |
| inclination: | 49.9859° |
| perigee height: | 613 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 53.5876° |
| argument of perigee: | 120.9109° |
| revolutions per day: | 14.83281787 |
| mean anomaly at epoch: | 239.2650° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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