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 59214U 26145.43901691 +.00000000 +00000-0 +55878-4 0 00002
2 59214 53.1601 157.8939 0001243 78.0838 282.0304 15.34396989 01
| Epoch (UTC): | 25 May 2026 10:32:11 |
| Eccentricity: | 0.0001243 |
| inclination: | 53.1601° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 157.8939° |
| argument of perigee: | 78.0838° |
| revolutions per day: | 15.34396989 |
| mean anomaly at epoch: | 282.0304° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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