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 54657U 26145.52491324 +.00000000 +00000-0 +19282-3 0 00003
2 54657 87.9252 248.4955 0002029 102.0281 258.1080 13.21825303 08
| Epoch (UTC): | 25 May 2026 12:35:52 |
| Eccentricity: | 0.0002029 |
| inclination: | 87.9252° |
| perigee height: | 1176 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 248.4955° |
| argument of perigee: | 102.0281° |
| revolutions per day: | 13.21825303 |
| mean anomaly at epoch: | 258.1080° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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