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 63835U 26145.44162303 +.00000000 +00000-0 +65230-3 0 00008
2 63835 97.3898 40.9248 0005246 184.1849 175.9351 15.33018177 07
| Epoch (UTC): | 25 May 2026 10:35:56 |
| Eccentricity: | 0.0005246 |
| inclination: | 97.3898° |
| perigee height: | 463 km |
| apogee height: | 470 km |
| right ascension of ascending node: | 40.9248° |
| argument of perigee: | 184.1849° |
| revolutions per day: | 15.33018177 |
| mean anomaly at epoch: | 175.9351° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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