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 63213U 26145.22343642 +.00000000 +00000-0 +54899-3 0 00000
2 63213 97.3933 41.5887 0003156 146.1812 213.9632 15.33682307 06
| Epoch (UTC): | 25 May 2026 05:21:44 |
| Eccentricity: | 0.0003156 |
| inclination: | 97.3933° |
| perigee height: | 463 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 41.5887° |
| argument of perigee: | 146.1812° |
| revolutions per day: | 15.33682307 |
| mean anomaly at epoch: | 213.9632° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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