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 62399U 26145.38550733 +.00000000 +00000-0 +67739-3 0 00009
2 62399 44.9984 23.9889 0006143 156.9206 203.1961 15.47011560 03
| Epoch (UTC): | 25 May 2026 09:15:07 |
| Eccentricity: | 0.0006143 |
| inclination: | 44.9984° |
| perigee height: | 421 km |
| apogee height: | 430 km |
| right ascension of ascending node: | 23.9889° |
| argument of perigee: | 156.9206° |
| revolutions per day: | 15.47011560 |
| mean anomaly at epoch: | 203.1961° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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