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 65539U 26145.44191591 +.00000000 +00000-0 -22643-3 0 00004
2 65539 97.4501 215.1366 0001547 186.7711 173.3496 15.05630663 06
| Epoch (UTC): | 25 May 2026 10:36:21 |
| Eccentricity: | 0.0001547 |
| inclination: | 97.4501° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 215.1366° |
| argument of perigee: | 186.7711° |
| revolutions per day: | 15.05630663 |
| mean anomaly at epoch: | 173.3496° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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