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 54118U 26145.46694185 +.00000000 +00000-0 +22535-3 0 00003
2 54118 87.9159 309.4939 0001786 96.2380 263.8956 13.19727499 08
| Epoch (UTC): | 25 May 2026 11:12:23 |
| Eccentricity: | 0.0001786 |
| inclination: | 87.9159° |
| perigee height: | 1184 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.4939° |
| argument of perigee: | 96.2380° |
| revolutions per day: | 13.19727499 |
| mean anomaly at epoch: | 263.8956° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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