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 65638U 26145.49314825 +.00000000 +00000-0 +60529-3 0 00000
2 65638 53.1599 309.3707 0001003 94.3535 265.7582 15.34409826 01
| Epoch (UTC): | 25 May 2026 11:50:08 |
| Eccentricity: | 0.0001003 |
| inclination: | 53.1599° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 309.3707° |
| argument of perigee: | 94.3535° |
| revolutions per day: | 15.34409826 |
| mean anomaly at epoch: | 265.7582° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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