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 54647U 26145.55688194 +.00000000 +00000-0 +23977-3 0 00004
2 54647 87.9254 248.4844 0002478 94.4911 265.6506 13.21826181 09
| Epoch (UTC): | 25 May 2026 13:21:54 |
| Eccentricity: | 0.0002478 |
| inclination: | 87.9254° |
| perigee height: | 1176 km |
| apogee height: | 1180 km |
| right ascension of ascending node: | 248.4844° |
| argument of perigee: | 94.4911° |
| revolutions per day: | 13.21826181 |
| mean anomaly at epoch: | 265.6506° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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