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 65655U 26145.08290588 +.00000000 +00000-0 -48465-3 0 00009
2 65655 97.4533 188.9527 0000742 188.0588 172.0627 15.05633954 07
| Epoch (UTC): | 25 May 2026 01:59:23 |
| Eccentricity: | 0.0000742 |
| inclination: | 97.4533° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 188.9527° |
| argument of perigee: | 188.0588° |
| revolutions per day: | 15.05633954 |
| mean anomaly at epoch: | 172.0627° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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