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 63214U 26145.43720551 +.00000000 +00000-0 +55200-3 0 00009
2 63214 97.3930 41.7568 0003126 146.2117 213.9326 15.33530146 01
| Epoch (UTC): | 25 May 2026 10:29:34 |
| Eccentricity: | 0.0003126 |
| inclination: | 97.3930° |
| perigee height: | 463 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 41.7568° |
| argument of perigee: | 146.2117° |
| revolutions per day: | 15.33530146 |
| mean anomaly at epoch: | 213.9326° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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