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 60720U 26145.30224441 +.00000000 +00000-0 +16361-4 0 00007
2 60720 53.1600 98.9009 0001143 66.9735 293.1403 15.69713657 04
| Epoch (UTC): | 25 May 2026 07:15:13 |
| Eccentricity: | 0.0001143 |
| inclination: | 53.1600° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 98.9009° |
| argument of perigee: | 66.9735° |
| revolutions per day: | 15.69713657 |
| mean anomaly at epoch: | 293.1403° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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