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 63516U 26145.39716156 +.00000000 +00000-0 +48275-3 0 00009
2 63516 53.1584 143.6233 0000906 81.2510 278.8594 15.31716476 07
| Epoch (UTC): | 25 May 2026 09:31:54 |
| Eccentricity: | 0.0000906 |
| inclination: | 53.1584° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 143.6233° |
| argument of perigee: | 81.2510° |
| revolutions per day: | 15.31716476 |
| mean anomaly at epoch: | 278.8594° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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