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 63282U 26145.54323155 +.00000000 +00000-0 +48132-3 0 00001
2 63282 43.0009 168.0356 0001725 263.0387 97.0269 15.27590469 03
| Epoch (UTC): | 25 May 2026 13:02:15 |
| Eccentricity: | 0.0001725 |
| inclination: | 43.0009° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 168.0356° |
| argument of perigee: | 263.0387° |
| revolutions per day: | 15.27590469 |
| mean anomaly at epoch: | 97.0269° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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