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 61017U 26145.61430786 +.00000000 +00000-0 +18259-3 0 00009
2 61017 49.9926 187.6575 0011786 305.1542 54.8292 14.84151993 03
| Epoch (UTC): | 25 May 2026 14:44:36 |
| Eccentricity: | 0.0011786 |
| inclination: | 49.9926° |
| perigee height: | 608 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 187.6575° |
| argument of perigee: | 305.1542° |
| revolutions per day: | 14.84151993 |
| mean anomaly at epoch: | 54.8292° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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