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 38652U 26145.08561955 +.00000000 +00000-0 +00000-0 0 00004
2 38652 0.0517 306.9145 0001982 111.6351 219.9281 1.00272696 00
| Epoch (UTC): | 25 May 2026 02:03:17 |
| Eccentricity: | 0.0001982 |
| inclination: | 0.0517° |
| perigee height: | 35778 km |
| apogee height: | 35795 km |
| right ascension of ascending node: | 306.9145° |
| argument of perigee: | 111.6351° |
| revolutions per day: | 1.00272696 |
| mean anomaly at epoch: | 219.9281° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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