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 60579U 26145.49879627 +.00000000 +00000-0 +68483-3 0 00002
2 60579 97.6841 228.0007 0003862 241.4984 118.5857 15.10383679 02
| Epoch (UTC): | 25 May 2026 11:58:15 |
| Eccentricity: | 0.0003862 |
| inclination: | 97.6841° |
| perigee height: | 532 km |
| apogee height: | 538 km |
| right ascension of ascending node: | 228.0007° |
| argument of perigee: | 241.4984° |
| revolutions per day: | 15.10383679 |
| mean anomaly at epoch: | 118.5857° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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