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 63144U 26145.44663559 +.00000000 +00000-0 +20749-2 0 00005
2 63144 42.9997 148.0808 0002019 251.5411 108.5237 15.70920524 01
| Epoch (UTC): | 25 May 2026 10:43:09 |
| Eccentricity: | 0.0002019 |
| inclination: | 42.9997° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 148.0808° |
| argument of perigee: | 251.5411° |
| revolutions per day: | 15.70920524 |
| mean anomaly at epoch: | 108.5237° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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