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 63562U 26145.43824870 +.00000000 +00000-0 +51349-3 0 00004
2 63562 42.9997 197.2954 0001226 274.0923 85.9788 15.27593400 00
| Epoch (UTC): | 25 May 2026 10:31:04 |
| Eccentricity: | 0.0001226 |
| inclination: | 42.9997° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 197.2954° |
| argument of perigee: | 274.0923° |
| revolutions per day: | 15.27593400 |
| mean anomaly at epoch: | 85.9788° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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