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 60747U 26145.63045149 +.00000000 +00000-0 +59476-3 0 00001
2 60747 97.6743 286.9169 0008868 224.3532 135.7004 15.40250658 00
| Epoch (UTC): | 25 May 2026 15:07:51 |
| Eccentricity: | 0.0008868 |
| inclination: | 97.6743° |
| perigee height: | 439 km |
| apogee height: | 451 km |
| right ascension of ascending node: | 286.9169° |
| argument of perigee: | 224.3532° |
| revolutions per day: | 15.40250658 |
| mean anomaly at epoch: | 135.7004° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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