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 63345U 26145.62265669 +.00000000 +00000-0 +16067-3 0 00007
2 63345 97.6096 327.0709 0015706 231.6594 128.3224 15.10867432 06
| Epoch (UTC): | 25 May 2026 14:56:37 |
| Eccentricity: | 0.0015706 |
| inclination: | 97.6096° |
| perigee height: | 523 km |
| apogee height: | 544 km |
| right ascension of ascending node: | 327.0709° |
| argument of perigee: | 231.6594° |
| revolutions per day: | 15.10867432 |
| mean anomaly at epoch: | 128.3224° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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