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 18316U 26150.28579188 +.00000000 +00000-0 +00000-0 0 00004
2 18316 12.8054 335.4343 0006517 64.0483 293.9014 0.99337359 06
| Epoch (UTC): | 30 May 2026 06:51:32 |
| Eccentricity: | 0.0006517 |
| inclination: | 12.8054° |
| perigee height: | 36023 km |
| apogee height: | 36078 km |
| right ascension of ascending node: | 335.4343° |
| argument of perigee: | 64.0483° |
| revolutions per day: | 0.99337359 |
| mean anomaly at epoch: | 293.9014° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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