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 39613U 26145.52354509 +.00000000 +00000-0 +00000-0 0 00006
2 39613 0.0106 317.5462 0000585 23.4417 146.6060 1.00275903 08
| Epoch (UTC): | 25 May 2026 12:33:54 |
| Eccentricity: | 0.0000585 |
| inclination: | 0.0106° |
| perigee height: | 35783 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 317.5462° |
| argument of perigee: | 23.4417° |
| revolutions per day: | 1.00275903 |
| mean anomaly at epoch: | 146.6060° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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