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 54120U 26145.40691154 +.00000000 +00000-0 +27552-3 0 00007
2 54120 87.9158 309.4945 0001793 85.0088 275.1249 13.19726539 01
| Epoch (UTC): | 25 May 2026 09:45:57 |
| Eccentricity: | 0.0001793 |
| inclination: | 87.9158° |
| perigee height: | 1184 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.4945° |
| argument of perigee: | 85.0088° |
| revolutions per day: | 13.19726539 |
| mean anomaly at epoch: | 275.1249° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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