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 65235U 26145.12309345 +.00000000 +00000-0 +18550-3 0 00001
2 65235 97.4485 188.0042 0002128 129.0556 231.0861 15.05655574 08
| Epoch (UTC): | 25 May 2026 02:57:15 |
| Eccentricity: | 0.0002128 |
| inclination: | 97.4485° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 188.0042° |
| argument of perigee: | 129.0556° |
| revolutions per day: | 15.05655574 |
| mean anomaly at epoch: | 231.0861° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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