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 61206U 26145.29727525 +.00000000 +00000-0 +11409-4 0 00004
2 61206 53.1587 158.4041 0001019 73.7125 286.4005 15.69710986 02
| Epoch (UTC): | 25 May 2026 07:08:04 |
| Eccentricity: | 0.0001019 |
| inclination: | 53.1587° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 158.4041° |
| argument of perigee: | 73.7125° |
| revolutions per day: | 15.69710986 |
| mean anomaly at epoch: | 286.4005° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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