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 66752U 26145.15040111 +.00000000 +00000-0 +14492-3 0 00003
2 66752 97.4191 217.4514 0002719 90.1056 270.0480 15.00031966 05
| Epoch (UTC): | 25 May 2026 03:36:34 |
| Eccentricity: | 0.0002719 |
| inclination: | 97.4191° |
| perigee height: | 565 km |
| apogee height: | 569 km |
| right ascension of ascending node: | 217.4514° |
| argument of perigee: | 90.1056° |
| revolutions per day: | 15.00031966 |
| mean anomaly at epoch: | 270.0480° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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