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 63352U 26145.38853030 +.00000000 +00000-0 +19481-3 0 00006
2 63352 97.5632 121.0100 0018032 349.1463 10.9376 15.13379996 01
| Epoch (UTC): | 25 May 2026 09:19:29 |
| Eccentricity: | 0.0018032 |
| inclination: | 97.5632° |
| perigee height: | 513 km |
| apogee height: | 538 km |
| right ascension of ascending node: | 121.0100° |
| argument of perigee: | 349.1463° |
| revolutions per day: | 15.13379996 |
| mean anomaly at epoch: | 10.9376° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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