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 59838U 26145.21592926 +.00000000 +00000-0 +40352-3 0 00007
2 59838 43.0019 201.9047 0001416 249.0690 111.0010 15.27609166 04
| Epoch (UTC): | 25 May 2026 05:10:56 |
| Eccentricity: | 0.0001416 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 201.9047° |
| argument of perigee: | 249.0690° |
| revolutions per day: | 15.27609166 |
| mean anomaly at epoch: | 111.0010° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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