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 63134U 26145.33009036 +.00000000 +00000-0 +12936-2 0 00005
2 63134 43.0007 148.9363 0002097 271.7430 88.3197 15.70859656 07
| Epoch (UTC): | 25 May 2026 07:55:19 |
| Eccentricity: | 0.0002097 |
| inclination: | 43.0007° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 148.9363° |
| argument of perigee: | 271.7430° |
| revolutions per day: | 15.70859656 |
| mean anomaly at epoch: | 88.3197° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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