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 66119U 26145.44605272 +.00000000 +00000-0 +66814-3 0 00002
2 66119 53.1611 42.9988 0001353 97.7163 262.3991 15.30210697 03
| Epoch (UTC): | 25 May 2026 10:42:18 |
| Eccentricity: | 0.0001353 |
| inclination: | 53.1611° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 42.9988° |
| argument of perigee: | 97.7163° |
| revolutions per day: | 15.30210697 |
| mean anomaly at epoch: | 262.3991° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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