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 61015U 26145.59237617 +.00000000 +00000-0 +23527-3 0 00006
2 61015 50.0017 188.1109 0013784 327.3812 32.6274 14.84122515 02
| Epoch (UTC): | 25 May 2026 14:13:01 |
| Eccentricity: | 0.0013784 |
| inclination: | 50.0017° |
| perigee height: | 607 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 188.1109° |
| argument of perigee: | 327.3812° |
| revolutions per day: | 14.84122515 |
| mean anomaly at epoch: | 32.6274° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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