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 39161U 26137.39309124 +.00000000 +00000-0 +13097-3 0 00006
2 39161 97.7313 192.6590 0009710 112.8919 247.3320 14.81297862 01
| Epoch (UTC): | 17 May 2026 09:26:03 |
| Eccentricity: | 0.0009710 |
| inclination: | 97.7313° |
| perigee height: | 618 km |
| apogee height: | 632 km |
| right ascension of ascending node: | 192.6590° |
| argument of perigee: | 112.8919° |
| revolutions per day: | 14.81297862 |
| mean anomaly at epoch: | 247.3320° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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