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 63125U 26145.57966109 +.00000000 +00000-0 +89617-5 0 00007
2 63125 97.3480 260.5285 0000900 101.5241 258.6096 15.21592355 05
| Epoch (UTC): | 25 May 2026 13:54:42 |
| Eccentricity: | 0.0000900 |
| inclination: | 97.3480° |
| perigee height: | 500 km |
| apogee height: | 502 km |
| right ascension of ascending node: | 260.5285° |
| argument of perigee: | 101.5241° |
| revolutions per day: | 15.21592355 |
| mean anomaly at epoch: | 258.6096° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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