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 67082U 26145.49301760 +.00000000 +00000-0 +16701-3 0 00002
2 67082 70.0014 180.7355 0004108 266.8711 93.1978 14.98335212 05
| Epoch (UTC): | 25 May 2026 11:49:56 |
| Eccentricity: | 0.0004108 |
| inclination: | 70.0014° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 180.7355° |
| argument of perigee: | 266.8711° |
| revolutions per day: | 14.98335212 |
| mean anomaly at epoch: | 93.1978° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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