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 63164U 26145.58990619 +.00000000 +00000-0 +36874-4 0 00000
2 63164 88.9691 303.0039 0015373 23.8328 336.3532 13.51007984 09
| Epoch (UTC): | 25 May 2026 14:09:27 |
| Eccentricity: | 0.0015373 |
| inclination: | 88.9691° |
| perigee height: | 1057 km |
| apogee height: | 1080 km |
| right ascension of ascending node: | 303.0039° |
| argument of perigee: | 23.8328° |
| revolutions per day: | 13.51007984 |
| mean anomaly at epoch: | 336.3532° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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