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 66927U 26145.03068670 +.00000000 +00000-0 +72384-3 0 00008
2 66927 53.1596 3.2384 0001060 96.2253 263.8870 15.34405858 02
| Epoch (UTC): | 25 May 2026 00:44:11 |
| Eccentricity: | 0.0001060 |
| inclination: | 53.1596° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 3.2384° |
| argument of perigee: | 96.2253° |
| revolutions per day: | 15.34405858 |
| mean anomaly at epoch: | 263.8870° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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