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 63470U 26145.46788348 +.00000000 +00000-0 +36870-3 0 00006
2 63470 42.9966 186.6311 0001440 273.9980 86.0707 15.27589906 01
| Epoch (UTC): | 25 May 2026 11:13:45 |
| Eccentricity: | 0.0001440 |
| inclination: | 42.9966° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 186.6311° |
| argument of perigee: | 273.9980° |
| revolutions per day: | 15.27589906 |
| mean anomaly at epoch: | 86.0707° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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