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 26066.45001424 +.00000000 +00000-0 +54259-3 0 00009
2 16614 98.7880 237.6523 4703125 301.2339 28.9921 5.50591817 03
| Epoch (UTC): | 07 March 2026 10:48:01 |
| Eccentricity: | 0.4703125 |
| inclination: | 98.7880° |
| perigee height: | 798 km |
| apogee height: | 13540 km |
| right ascension of ascending node: | 237.6523° |
| argument of perigee: | 301.2339° |
| revolutions per day: | 5.50591817 |
| mean anomaly at epoch: | 28.9921° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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