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 63882U 26144.99457248 +.00000000 +00000-0 +40446-3 0 00006
2 63882 70.0023 359.5461 0003339 270.6324 89.4475 15.41036032 08
| Epoch (UTC): | 24 May 2026 23:52:11 |
| Eccentricity: | 0.0003339 |
| inclination: | 70.0023° |
| perigee height: | 441 km |
| apogee height: | 445 km |
| right ascension of ascending node: | 359.5461° |
| argument of perigee: | 270.6324° |
| revolutions per day: | 15.41036032 |
| mean anomaly at epoch: | 89.4475° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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