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 63065U 26145.08441413 +.00000000 +00000-0 +38310-3 0 00004
2 63065 42.9974 75.6094 0001745 274.2782 85.7871 15.27601633 07
| Epoch (UTC): | 25 May 2026 02:01:33 |
| Eccentricity: | 0.0001745 |
| inclination: | 42.9974° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 75.6094° |
| argument of perigee: | 274.2782° |
| revolutions per day: | 15.27601633 |
| mean anomaly at epoch: | 85.7871° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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