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 65534U 26145.43082135 +.00000000 +00000-0 +45314-3 0 00000
2 65534 97.4467 215.0010 0001471 145.9381 214.1941 15.05656458 02
| Epoch (UTC): | 25 May 2026 10:20:22 |
| Eccentricity: | 0.0001471 |
| inclination: | 97.4467° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 215.0010° |
| argument of perigee: | 145.9381° |
| revolutions per day: | 15.05656458 |
| mean anomaly at epoch: | 214.1941° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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