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 63211U 26145.25054233 +.00000000 +00000-0 +60878-3 0 00000
2 63211 97.4009 42.4753 0004141 137.6752 222.4811 15.34940010 07
| Epoch (UTC): | 25 May 2026 06:00:46 |
| Eccentricity: | 0.0004141 |
| inclination: | 97.4009° |
| perigee height: | 458 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 42.4753° |
| argument of perigee: | 137.6752° |
| revolutions per day: | 15.34940010 |
| mean anomaly at epoch: | 222.4811° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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