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 39358U 26145.65085749 +.00000000 +00000-0 +15397-3 0 00001
2 39358 74.9736 39.3649 0016945 282.6771 77.2523 14.92545868 06
| Epoch (UTC): | 25 May 2026 15:37:14 |
| Eccentricity: | 0.0016945 |
| inclination: | 74.9736° |
| perigee height: | 578 km |
| apogee height: | 602 km |
| right ascension of ascending node: | 39.3649° |
| argument of perigee: | 282.6771° |
| revolutions per day: | 14.92545868 |
| mean anomaly at epoch: | 77.2523° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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