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 66931U 26145.31016972 +.00000000 +00000-0 +76163-3 0 00001
2 66931 53.1600 2.1380 0001205 93.5510 266.5630 15.34410855 01
| Epoch (UTC): | 25 May 2026 07:26:38 |
| Eccentricity: | 0.0001205 |
| inclination: | 53.1600° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 2.1380° |
| argument of perigee: | 93.5510° |
| revolutions per day: | 15.34410855 |
| mean anomaly at epoch: | 266.5630° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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