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 39199U 26142.85947302 +.00000000 +00000-0 +00000-0 0 00007
2 39199 35.6649 64.2334 0016619 185.3754 355.4646 1.00280263 09
| Epoch (UTC): | 22 May 2026 20:37:38 |
| Eccentricity: | 0.0016619 |
| inclination: | 35.6649° |
| perigee height: | 35714 km |
| apogee height: | 35854 km |
| right ascension of ascending node: | 64.2334° |
| argument of perigee: | 185.3754° |
| revolutions per day: | 1.00280263 |
| mean anomaly at epoch: | 355.4646° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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