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 67016U 26145.57322957 +.00000000 +00000-0 +11950-3 0 00000
2 67016 70.0008 260.6257 0003614 268.3820 91.6925 14.98334973 01
| Epoch (UTC): | 25 May 2026 13:45:27 |
| Eccentricity: | 0.0003614 |
| inclination: | 70.0008° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 260.6257° |
| argument of perigee: | 268.3820° |
| revolutions per day: | 14.98334973 |
| mean anomaly at epoch: | 91.6925° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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