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 63317U 26145.31716088 +.00000000 +00000-0 +15742-2 0 00006
2 63317 43.0000 162.2377 0001248 149.6700 210.4240 15.70865308 05
| Epoch (UTC): | 25 May 2026 07:36:42 |
| Eccentricity: | 0.0001248 |
| inclination: | 43.0000° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 162.2377° |
| argument of perigee: | 149.6700° |
| revolutions per day: | 15.70865308 |
| mean anomaly at epoch: | 210.4240° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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