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 63122U 26145.43843925 +.00000000 +00000-0 +80154-3 0 00004
2 63122 42.9953 299.4250 0000666 328.2541 31.8270 15.27617079 08
| Epoch (UTC): | 25 May 2026 10:31:21 |
| Eccentricity: | 0.0000666 |
| inclination: | 42.9953° |
| perigee height: | 482 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 299.4250° |
| argument of perigee: | 328.2541° |
| revolutions per day: | 15.27617079 |
| mean anomaly at epoch: | 31.8270° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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