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 65703U 26145.27975536 +.00000000 +00000-0 +47342-3 0 00009
2 65703 53.1606 349.6429 0001072 96.1933 263.9191 15.31715244 06
| Epoch (UTC): | 25 May 2026 06:42:50 |
| Eccentricity: | 0.0001072 |
| inclination: | 53.1606° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 349.6429° |
| argument of perigee: | 96.1933° |
| revolutions per day: | 15.31715244 |
| mean anomaly at epoch: | 263.9191° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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