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 63020U 26145.35573126 +.00000000 +00000-0 +11618-2 0 00003
2 63020 42.9940 263.2068 0000354 344.2756 15.8085 15.27587727 09
| Epoch (UTC): | 25 May 2026 08:32:15 |
| Eccentricity: | 0.0000354 |
| inclination: | 42.9940° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 263.2068° |
| argument of perigee: | 344.2756° |
| revolutions per day: | 15.27587727 |
| mean anomaly at epoch: | 15.8085° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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