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 54119U 26145.19369757 +.00000000 +00000-0 +14793-3 0 00005
2 54119 87.9159 309.5483 0001635 83.9725 276.1594 13.19725746 01
| Epoch (UTC): | 25 May 2026 04:38:55 |
| Eccentricity: | 0.0001635 |
| inclination: | 87.9159° |
| perigee height: | 1185 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.5483° |
| argument of perigee: | 83.9725° |
| revolutions per day: | 13.19725746 |
| mean anomaly at epoch: | 276.1594° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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