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 63130U 26145.14663566 +.00000000 +00000-0 +00000-0 0 00001
2 63130 65.0720 73.5848 0006025 231.9508 127.9858 2.13103804 03
| Epoch (UTC): | 25 May 2026 03:31:09 |
| Eccentricity: | 0.0006025 |
| inclination: | 65.0720° |
| perigee height: | 19114 km |
| apogee height: | 19145 km |
| right ascension of ascending node: | 73.5848° |
| argument of perigee: | 231.9508° |
| revolutions per day: | 2.13103804 |
| mean anomaly at epoch: | 127.9858° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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