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 66117U 26145.13636545 +.00000000 +00000-0 +65778-3 0 00001
2 66117 53.1583 44.6229 0001177 79.3083 280.8050 15.30201610 03
| Epoch (UTC): | 25 May 2026 03:16:21 |
| Eccentricity: | 0.0001177 |
| inclination: | 53.1583° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 44.6229° |
| argument of perigee: | 79.3083° |
| revolutions per day: | 15.30201610 |
| mean anomaly at epoch: | 280.8050° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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