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 66668U 26145.15347612 +.00000000 +00000-0 +10723-2 0 00007
2 66668 97.4056 219.5250 0008159 97.4978 262.7187 15.26335051 00
| Epoch (UTC): | 25 May 2026 03:41:00 |
| Eccentricity: | 0.0008159 |
| inclination: | 97.4056° |
| perigee height: | 481 km |
| apogee height: | 492 km |
| right ascension of ascending node: | 219.5250° |
| argument of perigee: | 97.4978° |
| revolutions per day: | 15.26335051 |
| mean anomaly at epoch: | 262.7187° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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