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 66277U 26145.40827439 +.00000000 +00000-0 +46986-3 0 00002
2 66277 53.1594 194.1019 0000879 79.3026 280.8075 15.34404462 06
| Epoch (UTC): | 25 May 2026 09:47:54 |
| Eccentricity: | 0.0000879 |
| inclination: | 53.1594° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 194.1019° |
| argument of perigee: | 79.3026° |
| revolutions per day: | 15.34404462 |
| mean anomaly at epoch: | 280.8075° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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