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 54145U 26145.37690567 +.00000000 +00000-0 +21650-3 0 00000
2 54145 87.9151 309.5218 0001606 88.2071 271.9246 13.19726938 09
| Epoch (UTC): | 25 May 2026 09:02:44 |
| Eccentricity: | 0.0001606 |
| inclination: | 87.9151° |
| perigee height: | 1185 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.5218° |
| argument of perigee: | 88.2071° |
| revolutions per day: | 13.19726938 |
| mean anomaly at epoch: | 271.9246° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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