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 63463U 26145.56524625 +.00000000 +00000-0 +41831-3 0 00008
2 63463 43.0021 185.6474 0001551 268.7773 91.2901 15.27590486 00
| Epoch (UTC): | 25 May 2026 13:33:57 |
| Eccentricity: | 0.0001551 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 185.6474° |
| argument of perigee: | 268.7773° |
| revolutions per day: | 15.27590486 |
| mean anomaly at epoch: | 91.2901° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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