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 63379U 26145.46819468 +.00000000 +00000-0 +92051-3 0 00005
2 63379 53.1613 55.1985 0004228 77.8056 282.3419 15.32158246 07
| Epoch (UTC): | 25 May 2026 11:14:12 |
| Eccentricity: | 0.0004228 |
| inclination: | 53.1613° |
| perigee height: | 466 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 55.1985° |
| argument of perigee: | 77.8056° |
| revolutions per day: | 15.32158246 |
| mean anomaly at epoch: | 282.3419° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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