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 62423U 26145.53149793 +.00000000 +00000-0 -32576-3 0 00006
2 62423 42.9990 240.2825 0000652 273.0727 87.0050 15.27577642 02
| Epoch (UTC): | 25 May 2026 12:45:21 |
| Eccentricity: | 0.0000652 |
| inclination: | 42.9990° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 240.2825° |
| argument of perigee: | 273.0727° |
| revolutions per day: | 15.27577642 |
| mean anomaly at epoch: | 87.0050° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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