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 63116U 26145.39582742 +.00000000 +00000-0 +16268-2 0 00003
2 63116 43.0005 134.0983 0001700 263.5051 96.5623 15.70903145 05
| Epoch (UTC): | 25 May 2026 09:29:59 |
| Eccentricity: | 0.0001700 |
| inclination: | 43.0005° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 134.0983° |
| argument of perigee: | 263.5051° |
| revolutions per day: | 15.70903145 |
| mean anomaly at epoch: | 96.5623° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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