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 63573U 26145.30248001 +.00000000 +00000-0 +93043-3 0 00005
2 63573 42.9978 249.3467 0001213 245.7084 114.3641 15.27581304 03
| Epoch (UTC): | 25 May 2026 07:15:34 |
| Eccentricity: | 0.0001213 |
| inclination: | 42.9978° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 249.3467° |
| argument of perigee: | 245.7084° |
| revolutions per day: | 15.27581304 |
| mean anomaly at epoch: | 114.3641° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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