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 63084U 26145.47192547 +.00000000 +00000-0 +25871-3 0 00007
2 63084 70.0004 160.8421 0003870 267.3030 92.7686 14.98338205 06
| Epoch (UTC): | 25 May 2026 11:19:34 |
| Eccentricity: | 0.0003870 |
| inclination: | 70.0004° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 160.8421° |
| argument of perigee: | 267.3030° |
| revolutions per day: | 14.98338205 |
| mean anomaly at epoch: | 92.7686° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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