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 59870U 26145.58772252 +.00000000 +00000-0 +78384-4 0 00002
2 59870 43.0006 199.6542 0001468 264.5850 95.4835 15.27576134 04
| Epoch (UTC): | 25 May 2026 14:06:19 |
| Eccentricity: | 0.0001468 |
| inclination: | 43.0006° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 199.6542° |
| argument of perigee: | 264.5850° |
| revolutions per day: | 15.27576134 |
| mean anomaly at epoch: | 95.4835° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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