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 66710U 26145.14925372 +.00000000 +00000-0 +28807-3 0 00002
2 66710 97.4191 219.0582 0003935 106.2388 253.9280 15.19734008 05
| Epoch (UTC): | 25 May 2026 03:34:55 |
| Eccentricity: | 0.0003935 |
| inclination: | 97.4191° |
| perigee height: | 504 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 219.0582° |
| argument of perigee: | 106.2388° |
| revolutions per day: | 15.19734008 |
| mean anomaly at epoch: | 253.9280° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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