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 61004U 26145.51570731 +.00000000 +00000-0 -68195-6 0 00007
2 61004 53.1611 68.6829 0001318 92.4412 267.6740 15.30187878 04
| Epoch (UTC): | 25 May 2026 12:22:37 |
| Eccentricity: | 0.0001318 |
| inclination: | 53.1611° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 68.6829° |
| argument of perigee: | 92.4412° |
| revolutions per day: | 15.30187878 |
| mean anomaly at epoch: | 267.6740° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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