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 59634U 26145.13146671 +.00000000 +00000-0 +48235-4 0 00003
2 59634 43.0014 68.0258 0001114 261.5533 98.5192 15.27575685 07
| Epoch (UTC): | 25 May 2026 03:09:18 |
| Eccentricity: | 0.0001114 |
| inclination: | 43.0014° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 68.0258° |
| argument of perigee: | 261.5533° |
| revolutions per day: | 15.27575685 |
| mean anomaly at epoch: | 98.5192° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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