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 63259U 26145.13224072 +.00000000 +00000-0 +28542-3 0 00001
2 63259 97.6957 38.2401 0002208 116.5294 243.6155 14.97412683 09
| Epoch (UTC): | 25 May 2026 03:10:25 |
| Eccentricity: | 0.0002208 |
| inclination: | 97.6957° |
| perigee height: | 573 km |
| apogee height: | 576 km |
| right ascension of ascending node: | 38.2401° |
| argument of perigee: | 116.5294° |
| revolutions per day: | 14.97412683 |
| mean anomaly at epoch: | 243.6155° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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