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 60541U 26145.18886788 +.00000000 +00000-0 +93323-3 0 00004
2 60541 97.6922 232.0088 0001397 121.9439 238.1930 15.17229840 00
| Epoch (UTC): | 25 May 2026 04:31:58 |
| Eccentricity: | 0.0001397 |
| inclination: | 97.6922° |
| perigee height: | 513 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 232.0088° |
| argument of perigee: | 121.9439° |
| revolutions per day: | 15.17229840 |
| mean anomaly at epoch: | 238.1930° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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