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 67213U 26145.49486774 +.00000000 +00000-0 +22734-3 0 00000
2 67213 70.0020 340.6293 0002849 266.2437 93.8396 14.98337675 01
| Epoch (UTC): | 25 May 2026 11:52:36 |
| Eccentricity: | 0.0002849 |
| inclination: | 70.0020° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 340.6293° |
| argument of perigee: | 266.2437° |
| revolutions per day: | 14.98337675 |
| mean anomaly at epoch: | 93.8396° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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