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 39455U 26145.61839803 +.00000000 +00000-0 +24390-4 0 00007
2 39455 98.0756 17.9303 0014673 17.9080 342.2625 14.43666921 08
| Epoch (UTC): | 25 May 2026 14:50:29 |
| Eccentricity: | 0.0014673 |
| inclination: | 98.0756° |
| perigee height: | 736 km |
| apogee height: | 757 km |
| right ascension of ascending node: | 17.9303° |
| argument of perigee: | 17.9080° |
| revolutions per day: | 14.43666921 |
| mean anomaly at epoch: | 342.2625° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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