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 66602U 26145.59068811 +.00000000 +00000-0 +97781-3 0 00004
2 66602 43.0006 342.1665 0000227 286.1678 73.9148 15.27596545 02
| Epoch (UTC): | 25 May 2026 14:10:35 |
| Eccentricity: | 0.0000227 |
| inclination: | 43.0006° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 342.1665° |
| argument of perigee: | 286.1678° |
| revolutions per day: | 15.27596545 |
| mean anomaly at epoch: | 73.9148° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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