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 54676U 26145.54173347 +.00000000 +00000-0 +35071-3 0 00002
2 54676 87.9254 248.4927 0001740 99.2999 260.8332 13.21825436 09
| Epoch (UTC): | 25 May 2026 13:00:05 |
| Eccentricity: | 0.0001740 |
| inclination: | 87.9254° |
| perigee height: | 1176 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 248.4927° |
| argument of perigee: | 99.2999° |
| revolutions per day: | 13.21825436 |
| mean anomaly at epoch: | 260.8332° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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