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 65537U 26145.15114870 +.00000000 +00000-0 -43686-3 0 00005
2 65537 97.4527 214.7598 0001966 219.9353 140.1730 15.05632391 03
| Epoch (UTC): | 25 May 2026 03:37:39 |
| Eccentricity: | 0.0001966 |
| inclination: | 97.4527° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 214.7598° |
| argument of perigee: | 219.9353° |
| revolutions per day: | 15.05632391 |
| mean anomaly at epoch: | 140.1730° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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