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 16597U 26150.45242323 +.00000000 +00000-0 +00000-0 0 00000
2 16597 12.2890 332.4258 0012451 223.5608 319.1715 0.99288738 09
| Epoch (UTC): | 30 May 2026 10:51:29 |
| Eccentricity: | 0.0012451 |
| inclination: | 12.2890° |
| perigee height: | 36012 km |
| apogee height: | 36117 km |
| right ascension of ascending node: | 332.4258° |
| argument of perigee: | 223.5608° |
| revolutions per day: | 0.99288738 |
| mean anomaly at epoch: | 319.1715° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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