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 59217U 26145.29612494 +.00000000 +00000-0 +19137-4 0 00007
2 59217 53.1610 158.4242 0001306 92.3707 267.7445 15.34388602 01
| Epoch (UTC): | 25 May 2026 07:06:25 |
| Eccentricity: | 0.0001306 |
| inclination: | 53.1610° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 158.4242° |
| argument of perigee: | 92.3707° |
| revolutions per day: | 15.34388602 |
| mean anomaly at epoch: | 267.7445° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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