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 12089U 26150.51488639 +.00000000 +00000-0 +00000-0 0 00001
2 12089 11.3172 327.1015 0009827 329.2527 7.9605 0.98889532 01
| Epoch (UTC): | 30 May 2026 12:21:26 |
| Eccentricity: | 0.0009827 |
| inclination: | 11.3172° |
| perigee height: | 36137 km |
| apogee height: | 36220 km |
| right ascension of ascending node: | 327.1015° |
| argument of perigee: | 329.2527° |
| revolutions per day: | 0.98889532 |
| mean anomaly at epoch: | 7.9605° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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