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 54132U 26145.42745523 +.00000000 +00000-0 +84972-4 0 00002
2 54132 87.9160 309.5017 0001901 96.3603 263.7747 13.19725749 05
| Epoch (UTC): | 25 May 2026 10:15:32 |
| Eccentricity: | 0.0001901 |
| inclination: | 87.9160° |
| perigee height: | 1184 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.5017° |
| argument of perigee: | 96.3603° |
| revolutions per day: | 13.19725749 |
| mean anomaly at epoch: | 263.7747° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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