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 63073U 26145.46742128 +.00000000 +00000-0 +84936-3 0 00007
2 63073 42.9997 66.3914 0000720 262.9134 97.1636 15.27590699 01
| Epoch (UTC): | 25 May 2026 11:13:05 |
| Eccentricity: | 0.0000720 |
| inclination: | 42.9997° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 66.3914° |
| argument of perigee: | 262.9134° |
| revolutions per day: | 15.27590699 |
| mean anomaly at epoch: | 97.1636° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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