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 16864U 26129.49400639 +.00000000 +00000-0 +56519-4 0 00003
2 16864 74.0287 199.7571 0032744 223.4774 136.3800 14.42306116 02
| Epoch (UTC): | 09 May 2026 11:51:22 |
| Eccentricity: | 0.0032744 |
| inclination: | 74.0287° |
| perigee height: | 728 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 199.7571° |
| argument of perigee: | 223.4774° |
| revolutions per day: | 14.42306116 |
| mean anomaly at epoch: | 136.3800° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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