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 63803U 26145.57566347 +.00000000 +00000-0 +59481-3 0 00004
2 63803 43.0035 338.0746 0000904 268.5643 91.5105 15.27589310 07
| Epoch (UTC): | 25 May 2026 13:48:57 |
| Eccentricity: | 0.0000904 |
| inclination: | 43.0035° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 338.0746° |
| argument of perigee: | 268.5643° |
| revolutions per day: | 15.27589310 |
| mean anomaly at epoch: | 91.5105° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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