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 63112U 26145.39064286 +.00000000 +00000-0 +14556-2 0 00005
2 63112 43.0003 134.9542 0002659 254.1645 105.8930 15.70862605 08
| Epoch (UTC): | 25 May 2026 09:22:31 |
| Eccentricity: | 0.0002659 |
| inclination: | 43.0003° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 134.9542° |
| argument of perigee: | 254.1645° |
| revolutions per day: | 15.70862605 |
| mean anomaly at epoch: | 105.8930° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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