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 54113U 26145.38954831 +.00000000 +00000-0 +17417-3 0 00009
2 54113 87.9159 309.5100 0001667 89.3724 270.7600 13.19726492 02
| Epoch (UTC): | 25 May 2026 09:20:56 |
| Eccentricity: | 0.0001667 |
| inclination: | 87.9159° |
| perigee height: | 1185 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.5100° |
| argument of perigee: | 89.3724° |
| revolutions per day: | 13.19726492 |
| mean anomaly at epoch: | 270.7600° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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