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 63673U 26145.44213897 +.00000000 +00000-0 +16179-2 0 00000
2 63673 43.0002 175.7192 0003220 274.7366 85.3133 15.70940420 05
| Epoch (UTC): | 25 May 2026 10:36:40 |
| Eccentricity: | 0.0003220 |
| inclination: | 43.0002° |
| perigee height: | 354 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 175.7192° |
| argument of perigee: | 274.7366° |
| revolutions per day: | 15.70940420 |
| mean anomaly at epoch: | 85.3133° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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