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 54643U 26145.54340962 +.00000000 +00000-0 +23166-3 0 00007
2 54643 87.9253 248.5046 0001766 97.6954 262.4380 13.21826068 09
| Epoch (UTC): | 25 May 2026 13:02:30 |
| Eccentricity: | 0.0001766 |
| inclination: | 87.9253° |
| perigee height: | 1176 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 248.5046° |
| argument of perigee: | 97.6954° |
| revolutions per day: | 13.21826068 |
| mean anomaly at epoch: | 262.4380° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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