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 54121U 26145.39586647 +.00000000 +00000-0 +22055-3 0 00009
2 54121 87.9160 309.5017 0002061 91.2042 268.9327 13.19726451 04
| Epoch (UTC): | 25 May 2026 09:30:02 |
| Eccentricity: | 0.0002061 |
| inclination: | 87.9160° |
| perigee height: | 1184 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.5017° |
| argument of perigee: | 91.2042° |
| revolutions per day: | 13.19726451 |
| mean anomaly at epoch: | 268.9327° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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