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 12658U 26108.50971299 +.00000000 +00000-0 +86939-3 0 00002
2 12658 82.9701 190.5327 0032736 256.0026 118.7430 14.29828876 09
| Epoch (UTC): | 18 April 2026 12:13:59 |
| Eccentricity: | 0.0032736 |
| inclination: | 82.9701° |
| perigee height: | 769 km |
| apogee height: | 816 km |
| right ascension of ascending node: | 190.5327° |
| argument of perigee: | 256.0026° |
| revolutions per day: | 14.29828876 |
| mean anomaly at epoch: | 118.7430° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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