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 67209U 26145.49074166 +.00000000 +00000-0 +77111-3 0 00002
2 67209 70.0025 341.0209 0002791 268.4385 91.6455 14.98329895 02
| Epoch (UTC): | 25 May 2026 11:46:40 |
| Eccentricity: | 0.0002791 |
| inclination: | 70.0025° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 341.0209° |
| argument of perigee: | 268.4385° |
| revolutions per day: | 14.98329895 |
| mean anomaly at epoch: | 91.6455° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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