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 65543U 26145.45298328 +.00000000 +00000-0 +32295-3 0 00009
2 65543 97.4516 215.1227 0000858 180.3363 179.7864 15.05652131 03
| Epoch (UTC): | 25 May 2026 10:52:17 |
| Eccentricity: | 0.0000858 |
| inclination: | 97.4516° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 215.1227° |
| argument of perigee: | 180.3363° |
| revolutions per day: | 15.05652131 |
| mean anomaly at epoch: | 179.7864° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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