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 63354U 26145.40524736 +.00000000 +00000-0 +23300-3 0 00004
2 63354 97.5684 121.6023 0018380 340.1306 19.9208 15.13884117 02
| Epoch (UTC): | 25 May 2026 09:43:33 |
| Eccentricity: | 0.0018380 |
| inclination: | 97.5684° |
| perigee height: | 512 km |
| apogee height: | 537 km |
| right ascension of ascending node: | 121.6023° |
| argument of perigee: | 340.1306° |
| revolutions per day: | 15.13884117 |
| mean anomaly at epoch: | 19.9208° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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