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 61047U 26145.46159529 +.00000000 +00000-0 +10164-3 0 00005
2 61047 52.9691 53.6157 0008809 57.0690 303.1150 15.20725749 06
| Epoch (UTC): | 25 May 2026 11:04:41 |
| Eccentricity: | 0.0008809 |
| inclination: | 52.9691° |
| perigee height: | 498 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 53.6157° |
| argument of perigee: | 57.0690° |
| revolutions per day: | 15.20725749 |
| mean anomaly at epoch: | 303.1150° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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