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 66939U 26145.30385650 +.00000000 +00000-0 +47673-3 0 00004
2 66939 53.1592 2.0939 0001231 56.4763 303.6357 15.34431371 00
| Epoch (UTC): | 25 May 2026 07:17:33 |
| Eccentricity: | 0.0001231 |
| inclination: | 53.1592° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 2.0939° |
| argument of perigee: | 56.4763° |
| revolutions per day: | 15.34431371 |
| mean anomaly at epoch: | 303.6357° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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