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 63646U 26145.42387339 +.00000000 +00000-0 +80689-3 0 00009
2 63646 42.9961 291.7396 0000859 297.1262 62.9502 15.27598031 01
| Epoch (UTC): | 25 May 2026 10:10:22 |
| Eccentricity: | 0.0000859 |
| inclination: | 42.9961° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 291.7396° |
| argument of perigee: | 297.1262° |
| revolutions per day: | 15.27598031 |
| mean anomaly at epoch: | 62.9502° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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