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 66175U 26145.55288803 +.00000000 +00000-0 +23632-3 0 00004
2 66175 97.4126 221.3255 0002388 98.7188 261.4320 15.25430307 06
| Epoch (UTC): | 25 May 2026 13:16:09 |
| Eccentricity: | 0.0002388 |
| inclination: | 97.4126° |
| perigee height: | 488 km |
| apogee height: | 491 km |
| right ascension of ascending node: | 221.3255° |
| argument of perigee: | 98.7188° |
| revolutions per day: | 15.25430307 |
| mean anomaly at epoch: | 261.4320° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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