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 63668U 26145.46869267 +.00000000 +00000-0 +12339-2 0 00008
2 63668 43.0000 175.9346 0000634 259.7067 100.3729 15.70860428 05
| Epoch (UTC): | 25 May 2026 11:14:55 |
| Eccentricity: | 0.0000634 |
| inclination: | 43.0000° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 175.9346° |
| argument of perigee: | 259.7067° |
| revolutions per day: | 15.70860428 |
| mean anomaly at epoch: | 100.3729° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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