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 54677U 26145.51818451 +.00000000 +00000-0 +26181-3 0 00004
2 54677 87.9252 248.4991 0002014 92.8532 267.2833 13.21825593 07
| Epoch (UTC): | 25 May 2026 12:26:11 |
| Eccentricity: | 0.0002014 |
| inclination: | 87.9252° |
| perigee height: | 1176 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 248.4991° |
| argument of perigee: | 92.8532° |
| revolutions per day: | 13.21825593 |
| mean anomaly at epoch: | 267.2833° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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