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 60723U 26145.28262716 +.00000000 +00000-0 +17270-4 0 00004
2 60723 53.1596 98.7676 0001098 89.8110 270.3033 15.69706279 07
| Epoch (UTC): | 25 May 2026 06:46:58 |
| Eccentricity: | 0.0001098 |
| inclination: | 53.1596° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 98.7676° |
| argument of perigee: | 89.8110° |
| revolutions per day: | 15.69706279 |
| mean anomaly at epoch: | 270.3033° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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