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 62415U 26145.05735912 +.00000000 +00000-0 +13077-2 0 00001
2 62415 42.9994 67.1136 0002167 250.0069 110.0566 15.70846554 03
| Epoch (UTC): | 25 May 2026 01:22:35 |
| Eccentricity: | 0.0002167 |
| inclination: | 42.9994° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 67.1136° |
| argument of perigee: | 250.0069° |
| revolutions per day: | 15.70846554 |
| mean anomaly at epoch: | 110.0566° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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