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 54109U 26145.52224648 +.00000000 +00000-0 +23173-3 0 00002
2 54109 96.9205 205.3781 0011976 107.5026 252.7537 15.51047327 09
| Epoch (UTC): | 25 May 2026 12:32:02 |
| Eccentricity: | 0.0011976 |
| inclination: | 96.9205° |
| perigee height: | 406 km |
| apogee height: | 422 km |
| right ascension of ascending node: | 205.3781° |
| argument of perigee: | 107.5026° |
| revolutions per day: | 15.51047327 |
| mean anomaly at epoch: | 252.7537° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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