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 63476U 26145.47801416 +.00000000 +00000-0 +54355-3 0 00003
2 63476 42.9990 185.8365 0001574 281.6171 78.4504 15.27594553 04
| Epoch (UTC): | 25 May 2026 11:28:20 |
| Eccentricity: | 0.0001574 |
| inclination: | 42.9990° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 185.8365° |
| argument of perigee: | 281.6171° |
| revolutions per day: | 15.27594553 |
| mean anomaly at epoch: | 78.4504° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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