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 63499U 26145.37383115 +.00000000 +00000-0 +43559-3 0 00002
2 63499 53.1588 143.5187 0001156 85.4505 274.6629 15.31709668 04
| Epoch (UTC): | 25 May 2026 08:58:19 |
| Eccentricity: | 0.0001156 |
| inclination: | 53.1588° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 143.5187° |
| argument of perigee: | 85.4505° |
| revolutions per day: | 15.31709668 |
| mean anomaly at epoch: | 274.6629° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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