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 16409U 26064.70608687 +.00000000 +00000-0 +32490-4 0 00005
2 16409 82.5416 344.7647 0016252 84.7337 275.5677 13.84923174 02
| Epoch (UTC): | 05 March 2026 16:56:45 |
| Eccentricity: | 0.0016252 |
| inclination: | 82.5416° |
| perigee height: | 935 km |
| apogee height: | 958 km |
| right ascension of ascending node: | 344.7647° |
| argument of perigee: | 84.7337° |
| revolutions per day: | 13.84923174 |
| mean anomaly at epoch: | 275.5677° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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