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 54675U 26145.56190366 +.00000000 +00000-0 -29035-3 0 00007
2 54675 87.9265 248.4720 0002160 98.7262 261.4117 13.21827430 09
| Epoch (UTC): | 25 May 2026 13:29:08 |
| Eccentricity: | 0.0002160 |
| inclination: | 87.9265° |
| perigee height: | 1176 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 248.4720° |
| argument of perigee: | 98.7262° |
| revolutions per day: | 13.21827430 |
| mean anomaly at epoch: | 261.4117° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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