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 63208U 26145.54910139 +.00000000 +00000-0 +37590-3 0 00009
2 63208 97.4516 224.9710 0001166 136.2367 223.8963 15.24651928 06
| Epoch (UTC): | 25 May 2026 13:10:42 |
| Eccentricity: | 0.0001166 |
| inclination: | 97.4516° |
| perigee height: | 491 km |
| apogee height: | 493 km |
| right ascension of ascending node: | 224.9710° |
| argument of perigee: | 136.2367° |
| revolutions per day: | 15.24651928 |
| mean anomaly at epoch: | 223.8963° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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