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 63484U 26145.42805907 +.00000000 +00000-0 +47786-3 0 00006
2 63484 43.0020 186.3117 0001250 275.3561 84.7148 15.27574465 08
| Epoch (UTC): | 25 May 2026 10:16:24 |
| Eccentricity: | 0.0001250 |
| inclination: | 43.0020° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 186.3117° |
| argument of perigee: | 275.3561° |
| revolutions per day: | 15.27574465 |
| mean anomaly at epoch: | 84.7148° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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