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 26161.58896878 +.00000000 +00000-0 +33959-5 0 00002
2 16409 82.5374 267.5989 0015220 167.2648 192.8900 13.84927489 05
| Epoch (UTC): | 10 June 2026 14:08:06 |
| Eccentricity: | 0.0015220 |
| inclination: | 82.5374° |
| perigee height: | 935 km |
| apogee height: | 958 km |
| right ascension of ascending node: | 267.5989° |
| argument of perigee: | 167.2648° |
| revolutions per day: | 13.84927489 |
| mean anomaly at epoch: | 192.8900° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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