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 63146U 26145.51900209 +.00000000 +00000-0 +76438-3 0 00008
2 63146 43.0007 309.1383 0001437 254.2998 105.7695 15.27587457 01
| Epoch (UTC): | 25 May 2026 12:27:21 |
| Eccentricity: | 0.0001437 |
| inclination: | 43.0007° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 309.1383° |
| argument of perigee: | 254.2998° |
| revolutions per day: | 15.27587457 |
| mean anomaly at epoch: | 105.7695° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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