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 18129U 26112.13536919 +.00000000 +00000-0 +53492-4 0 00000
2 18129 82.9295 4.3376 0012926 107.2936 57.5858 13.73262333 00
| Epoch (UTC): | 22 April 2026 03:14:55 |
| Eccentricity: | 0.0012926 |
| inclination: | 82.9295° |
| perigee height: | 978 km |
| apogee height: | 997 km |
| right ascension of ascending node: | 4.3376° |
| argument of perigee: | 107.2936° |
| revolutions per day: | 13.73262333 |
| mean anomaly at epoch: | 57.5858° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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