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 60550U 26145.11534080 +.00000000 +00000-0 +10393-3 0 00008
2 60550 97.6758 221.3993 0007308 140.6289 219.5466 14.97963137 00
| Epoch (UTC): | 25 May 2026 02:46:05 |
| Eccentricity: | 0.0007308 |
| inclination: | 97.6758° |
| perigee height: | 568 km |
| apogee height: | 578 km |
| right ascension of ascending node: | 221.3993° |
| argument of perigee: | 140.6289° |
| revolutions per day: | 14.97963137 |
| mean anomaly at epoch: | 219.5466° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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