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 66392U 26145.21101976 +.00000000 +00000-0 +58351-3 0 00009
2 66392 53.1592 221.2765 0001304 90.8248 269.2902 15.30208242 04
| Epoch (UTC): | 25 May 2026 05:03:52 |
| Eccentricity: | 0.0001304 |
| inclination: | 53.1592° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 221.2765° |
| argument of perigee: | 90.8248° |
| revolutions per day: | 15.30208242 |
| mean anomaly at epoch: | 269.2902° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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