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 61060U 26144.82103819 +.00000000 +00000-0 +19474-4 0 00004
2 61060 53.1565 296.1510 0001123 109.1862 250.9277 15.69711717 05
| Epoch (UTC): | 24 May 2026 19:42:17 |
| Eccentricity: | 0.0001123 |
| inclination: | 53.1565° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 296.1510° |
| argument of perigee: | 109.1862° |
| revolutions per day: | 15.69711717 |
| mean anomaly at epoch: | 250.9277° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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