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 16614U 26111.31999551 +.00000000 +00000-0 +21213-3 0 00006
2 16614 98.7888 245.7378 4696193 277.9050 47.4795 5.50594080 04
| Epoch (UTC): | 21 April 2026 07:40:47 |
| Eccentricity: | 0.4696193 |
| inclination: | 98.7888° |
| perigee height: | 807 km |
| apogee height: | 13531 km |
| right ascension of ascending node: | 245.7378° |
| argument of perigee: | 277.9050° |
| revolutions per day: | 5.50594080 |
| mean anomaly at epoch: | 47.4795° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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