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 66659U 26145.30246096 +.00000000 +00000-0 +17625-3 0 00007
2 66659 97.7486 75.0196 0015044 93.5377 266.7564 14.93729379 01
| Epoch (UTC): | 25 May 2026 07:15:32 |
| Eccentricity: | 0.0015044 |
| inclination: | 97.7486° |
| perigee height: | 576 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 75.0196° |
| argument of perigee: | 93.5377° |
| revolutions per day: | 14.93729379 |
| mean anomaly at epoch: | 266.7564° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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