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 63481U 26145.44009499 +.00000000 +00000-0 +58868-3 0 00000
2 63481 43.0019 182.9327 0002002 283.9741 76.0888 15.27597548 01
| Epoch (UTC): | 25 May 2026 10:33:44 |
| Eccentricity: | 0.0002002 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 182.9327° |
| argument of perigee: | 283.9741° |
| revolutions per day: | 15.27597548 |
| mean anomaly at epoch: | 76.0888° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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