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 62595U 26145.02167806 +.00000000 +00000-0 +64848-3 0 00001
2 62595 43.0007 25.6674 0001853 263.2261 96.8396 15.70868509 02
| Epoch (UTC): | 25 May 2026 00:31:12 |
| Eccentricity: | 0.0001853 |
| inclination: | 43.0007° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 25.6674° |
| argument of perigee: | 263.2261° |
| revolutions per day: | 15.70868509 |
| mean anomaly at epoch: | 96.8396° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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