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 63040U 26145.05819602 +.00000000 +00000-0 +43589-3 0 00007
2 63040 53.1583 263.0867 0000892 67.6255 292.4841 15.31716861 01
| Epoch (UTC): | 25 May 2026 01:23:48 |
| Eccentricity: | 0.0000892 |
| inclination: | 53.1583° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 263.0867° |
| argument of perigee: | 67.6255° |
| revolutions per day: | 15.31716861 |
| mean anomaly at epoch: | 292.4841° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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