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 39150U 26145.63193043 +.00000000 +00000-0 +13906-3 0 00000
2 39150 97.9095 218.1575 0016591 343.7504 16.3172 14.76548216 00
| Epoch (UTC): | 25 May 2026 15:09:58 |
| Eccentricity: | 0.0016591 |
| inclination: | 97.9095° |
| perigee height: | 629 km |
| apogee height: | 652 km |
| right ascension of ascending node: | 218.1575° |
| argument of perigee: | 343.7504° |
| revolutions per day: | 14.76548216 |
| mean anomaly at epoch: | 16.3172° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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