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 63346U 26145.61422956 +.00000000 +00000-0 +15622-3 0 00007
2 63346 97.6122 327.2381 0014743 230.9766 129.0152 15.10861225 00
| Epoch (UTC): | 25 May 2026 14:44:29 |
| Eccentricity: | 0.0014743 |
| inclination: | 97.6122° |
| perigee height: | 523 km |
| apogee height: | 544 km |
| right ascension of ascending node: | 327.2381° |
| argument of perigee: | 230.9766° |
| revolutions per day: | 15.10861225 |
| mean anomaly at epoch: | 129.0152° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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