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 67028U 26145.38981110 +.00000000 +00000-0 +23163-3 0 00003
2 67028 70.0005 261.1865 0003378 268.9670 91.1102 14.98335446 06
| Epoch (UTC): | 25 May 2026 09:21:19 |
| Eccentricity: | 0.0003378 |
| inclination: | 70.0005° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 261.1865° |
| argument of perigee: | 268.9670° |
| revolutions per day: | 14.98335446 |
| mean anomaly at epoch: | 91.1102° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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