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 61666U 26145.27025037 +.00000000 +00000-0 -82203-5 0 00003
2 61666 53.1599 95.1425 0001333 74.1722 285.9426 15.30218711 03
| Epoch (UTC): | 25 May 2026 06:29:09 |
| Eccentricity: | 0.0001333 |
| inclination: | 53.1599° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 95.1425° |
| argument of perigee: | 74.1722° |
| revolutions per day: | 15.30218711 |
| mean anomaly at epoch: | 285.9426° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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