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 63311U 26145.50272652 +.00000000 +00000-0 +11734-2 0 00002
2 63311 43.0003 161.9451 0002612 236.8148 123.2470 15.70862566 01
| Epoch (UTC): | 25 May 2026 12:03:55 |
| Eccentricity: | 0.0002612 |
| inclination: | 43.0003° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 161.9451° |
| argument of perigee: | 236.8148° |
| revolutions per day: | 15.70862566 |
| mean anomaly at epoch: | 123.2470° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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