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 59444U 26145.01366002 +.00000000 +00000-0 +89215-3 0 00003
2 59444 45.6051 17.5519 0006584 189.5359 170.5404 15.13118521 09
| Epoch (UTC): | 25 May 2026 00:19:40 |
| Eccentricity: | 0.0006584 |
| inclination: | 45.6051° |
| perigee height: | 522 km |
| apogee height: | 531 km |
| right ascension of ascending node: | 17.5519° |
| argument of perigee: | 189.5359° |
| revolutions per day: | 15.13118521 |
| mean anomaly at epoch: | 170.5404° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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