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 67083U 26145.38455845 +.00000000 +00000-0 +29626-3 0 00005
2 67083 70.0007 181.1516 0002697 279.1779 80.9074 14.98339297 02
| Epoch (UTC): | 25 May 2026 09:13:45 |
| Eccentricity: | 0.0002697 |
| inclination: | 70.0007° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 181.1516° |
| argument of perigee: | 279.1779° |
| revolutions per day: | 14.98339297 |
| mean anomaly at epoch: | 80.9074° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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