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 39634U 26142.72179622 +.00000000 +00000-0 -12848-5 0 00008
2 39634 98.1786 150.6264 0001414 83.6628 276.4733 14.59199537 08
| Epoch (UTC): | 22 May 2026 17:19:23 |
| Eccentricity: | 0.0001414 |
| inclination: | 98.1786° |
| perigee height: | 695 km |
| apogee height: | 697 km |
| right ascension of ascending node: | 150.6264° |
| argument of perigee: | 83.6628° |
| revolutions per day: | 14.59199537 |
| mean anomaly at epoch: | 276.4733° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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