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 66864U 26145.39461416 +.00000000 +00000-0 +72608-3 0 00001
2 66864 42.9979 270.5368 0000367 155.6727 204.4142 15.27603569 03
| Epoch (UTC): | 25 May 2026 09:28:14 |
| Eccentricity: | 0.0000367 |
| inclination: | 42.9979° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 270.5368° |
| argument of perigee: | 155.6727° |
| revolutions per day: | 15.27603569 |
| mean anomaly at epoch: | 204.4142° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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