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 16624U 26140.58966334 +.00000000 +00000-0 +22509-3 0 00000
2 16624 63.2983 191.5063 0795851 115.7570 252.7778 13.71853486 02
| Epoch (UTC): | 20 May 2026 14:09:06 |
| Eccentricity: | 0.0795851 |
| inclination: | 63.2983° |
| perigee height: | 406 km |
| apogee height: | 1580 km |
| right ascension of ascending node: | 191.5063° |
| argument of perigee: | 115.7570° |
| revolutions per day: | 13.71853486 |
| mean anomaly at epoch: | 252.7778° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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