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 63085U 26145.43454281 +.00000000 +00000-0 -10854-3 0 00006
2 63085 70.0000 161.1149 0004299 267.7715 92.2952 14.98329874 07
| Epoch (UTC): | 25 May 2026 10:25:44 |
| Eccentricity: | 0.0004299 |
| inclination: | 70.0000° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 161.1149° |
| argument of perigee: | 267.7715° |
| revolutions per day: | 14.98329874 |
| mean anomaly at epoch: | 92.2952° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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