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 63913U 26145.35900634 +.00000000 +00000-0 +62682-3 0 00000
2 63913 43.0013 103.2009 0001546 262.0283 98.0394 15.27600564 08
| Epoch (UTC): | 25 May 2026 08:36:58 |
| Eccentricity: | 0.0001546 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 103.2009° |
| argument of perigee: | 262.0283° |
| revolutions per day: | 15.27600564 |
| mean anomaly at epoch: | 98.0394° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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