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 65523U 26145.14283852 +.00000000 +00000-0 +22463-3 0 00005
2 65523 97.4497 214.7688 0001446 207.2327 152.8825 15.05645620 02
| Epoch (UTC): | 25 May 2026 03:25:41 |
| Eccentricity: | 0.0001446 |
| inclination: | 97.4497° |
| perigee height: | 549 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 214.7688° |
| argument of perigee: | 207.2327° |
| revolutions per day: | 15.05645620 |
| mean anomaly at epoch: | 152.8825° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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