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 63106U 26145.44892345 +.00000000 +00000-0 +14187-2 0 00009
2 63106 43.0001 134.5307 0001078 258.5927 101.4820 15.70874771 06
| Epoch (UTC): | 25 May 2026 10:46:26 |
| Eccentricity: | 0.0001078 |
| inclination: | 43.0001° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 134.5307° |
| argument of perigee: | 258.5927° |
| revolutions per day: | 15.70874771 |
| mean anomaly at epoch: | 101.4820° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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