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 60501U 26135.22525480 +.00000000 +00000-0 +24138-3 0 00001
2 60501 97.3705 219.0244 0004170 56.2555 303.9089 15.41837298 07
| Epoch (UTC): | 15 May 2026 05:24:22 |
| Eccentricity: | 0.0004170 |
| inclination: | 97.3705° |
| perigee height: | 438 km |
| apogee height: | 444 km |
| right ascension of ascending node: | 219.0244° |
| argument of perigee: | 56.2555° |
| revolutions per day: | 15.41837298 |
| mean anomaly at epoch: | 303.9089° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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