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 65535U 26145.11792014 +.00000000 +00000-0 +38295-3 0 00000
2 65535 97.4485 214.8051 0002579 118.8244 241.3242 15.05663950 03
| Epoch (UTC): | 25 May 2026 02:49:48 |
| Eccentricity: | 0.0002579 |
| inclination: | 97.4485° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 214.8051° |
| argument of perigee: | 118.8244° |
| revolutions per day: | 15.05663950 |
| mean anomaly at epoch: | 241.3242° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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