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 63109U 26145.43830154 +.00000000 +00000-0 +15322-2 0 00003
2 63109 43.0011 134.4435 0002310 257.4515 102.6094 15.70897631 08
| Epoch (UTC): | 25 May 2026 10:31:09 |
| Eccentricity: | 0.0002310 |
| inclination: | 43.0011° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 134.4435° |
| argument of perigee: | 257.4515° |
| revolutions per day: | 15.70897631 |
| mean anomaly at epoch: | 102.6094° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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