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 39157U 26145.46054689 +.00000000 +00000-0 +00000-0 0 00008
2 39157 0.0143 315.0685 0002121 99.6807 91.9725 1.00273514 04
| Epoch (UTC): | 25 May 2026 11:03:11 |
| Eccentricity: | 0.0002121 |
| inclination: | 0.0143° |
| perigee height: | 35777 km |
| apogee height: | 35795 km |
| right ascension of ascending node: | 315.0685° |
| argument of perigee: | 99.6807° |
| revolutions per day: | 1.00273514 |
| mean anomaly at epoch: | 91.9725° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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