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 66681U 26145.16247550 +.00000000 +00000-0 +70880-3 0 00004
2 66681 97.4121 219.3590 0006864 102.5481 257.6524 15.23164777 01
| Epoch (UTC): | 25 May 2026 03:53:57 |
| Eccentricity: | 0.0006864 |
| inclination: | 97.4121° |
| perigee height: | 492 km |
| apogee height: | 501 km |
| right ascension of ascending node: | 219.3590° |
| argument of perigee: | 102.5481° |
| revolutions per day: | 15.23164777 |
| mean anomaly at epoch: | 257.6524° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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