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 39635U 26139.86086404 +.00000000 +00000-0 +00000-0 0 00006
2 39635 28.9733 240.8911 0024227 185.2284 176.5740 1.00280229 06
| Epoch (UTC): | 19 May 2026 20:39:38 |
| Eccentricity: | 0.0024227 |
| inclination: | 28.9733° |
| perigee height: | 35682 km |
| apogee height: | 35886 km |
| right ascension of ascending node: | 240.8911° |
| argument of perigee: | 185.2284° |
| revolutions per day: | 1.00280229 |
| mean anomaly at epoch: | 176.5740° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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