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 12092U 26088.17249774 +.00000000 +00000-0 +36118-4 0 00005
2 12092 82.9449 19.4490 0030964 124.9462 347.6637 13.77362052 01
| Epoch (UTC): | 29 March 2026 04:08:23 |
| Eccentricity: | 0.0030964 |
| inclination: | 82.9449° |
| perigee height: | 950 km |
| apogee height: | 996 km |
| right ascension of ascending node: | 19.4490° |
| argument of perigee: | 124.9462° |
| revolutions per day: | 13.77362052 |
| mean anomaly at epoch: | 347.6637° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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