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 65540U 26145.45852066 +.00000000 +00000-0 +32285-3 0 00000
2 65540 97.4475 215.1177 0002637 132.7675 227.3774 15.05658802 03
| Epoch (UTC): | 25 May 2026 11:00:16 |
| Eccentricity: | 0.0002637 |
| inclination: | 97.4475° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 215.1177° |
| argument of perigee: | 132.7675° |
| revolutions per day: | 15.05658802 |
| mean anomaly at epoch: | 227.3774° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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