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 18877U 26150.08961882 +.00000000 +00000-0 +00000-0 0 00000
2 18877 15.2289 351.8431 0008805 333.0597 27.1970 0.98134377 04
| Epoch (UTC): | 30 May 2026 02:09:03 |
| Eccentricity: | 0.0008805 |
| inclination: | 15.2289° |
| perigee height: | 36359 km |
| apogee height: | 36434 km |
| right ascension of ascending node: | 351.8431° |
| argument of perigee: | 333.0597° |
| revolutions per day: | 0.98134377 |
| mean anomaly at epoch: | 27.1970° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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