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 66130U 26145.13319836 +.00000000 +00000-0 +60412-3 0 00007
2 66130 53.1590 44.6007 0001112 101.2517 258.8609 15.30199494 07
| Epoch (UTC): | 25 May 2026 03:11:48 |
| Eccentricity: | 0.0001112 |
| inclination: | 53.1590° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 44.6007° |
| argument of perigee: | 101.2517° |
| revolutions per day: | 15.30199494 |
| mean anomaly at epoch: | 258.8609° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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