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 62478U 26145.13154409 +.00000000 +00000-0 +43143-3 0 00003
2 62478 43.0007 304.6740 0001380 274.0513 86.0181 15.27581223 01
| Epoch (UTC): | 25 May 2026 03:09:25 |
| Eccentricity: | 0.0001380 |
| inclination: | 43.0007° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 304.6740° |
| argument of perigee: | 274.0513° |
| revolutions per day: | 15.27581223 |
| mean anomaly at epoch: | 86.0181° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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