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 63513U 26145.38316022 +.00000000 +00000-0 +41901-3 0 00002
2 63513 53.1600 143.5387 0001223 80.9504 279.1636 15.31714771 01
| Epoch (UTC): | 25 May 2026 09:11:45 |
| Eccentricity: | 0.0001223 |
| inclination: | 53.1600° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 143.5387° |
| argument of perigee: | 80.9504° |
| revolutions per day: | 15.31714771 |
| mean anomaly at epoch: | 279.1636° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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