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 61601U 26145.33855977 +.00000000 +00000-0 -13821-4 0 00002
2 61601 87.9144 10.4423 0002126 61.9424 298.1923 13.17650559 06
| Epoch (UTC): | 25 May 2026 08:07:31 |
| Eccentricity: | 0.0002126 |
| inclination: | 87.9144° |
| perigee height: | 1192 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.4423° |
| argument of perigee: | 61.9424° |
| revolutions per day: | 13.17650559 |
| mean anomaly at epoch: | 298.1923° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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