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 60461U 26145.67793545 +.00000000 +00000-0 +23111-3 0 00005
2 60461 35.0043 291.4894 0002988 334.4361 25.6207 15.29516066 05
| Epoch (UTC): | 25 May 2026 16:16:13 |
| Eccentricity: | 0.0002988 |
| inclination: | 35.0043° |
| perigee height: | 475 km |
| apogee height: | 479 km |
| right ascension of ascending node: | 291.4894° |
| argument of perigee: | 334.4361° |
| revolutions per day: | 15.29516066 |
| mean anomaly at epoch: | 25.6207° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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