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 63080U 26145.43874154 +.00000000 +00000-0 +44567-3 0 00003
2 63080 70.0001 161.1273 0003131 267.9849 92.0952 14.98334184 03
| Epoch (UTC): | 25 May 2026 10:31:47 |
| Eccentricity: | 0.0003131 |
| inclination: | 70.0001° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 161.1273° |
| argument of perigee: | 267.9849° |
| revolutions per day: | 14.98334184 |
| mean anomaly at epoch: | 92.0952° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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