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 67212U 26145.50739832 +.00000000 +00000-0 +32674-3 0 00001
2 67212 70.0020 340.6723 0003126 263.4323 96.6481 14.98320915 05
| Epoch (UTC): | 25 May 2026 12:10:39 |
| Eccentricity: | 0.0003126 |
| inclination: | 70.0020° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 340.6723° |
| argument of perigee: | 263.4323° |
| revolutions per day: | 14.98320915 |
| mean anomaly at epoch: | 96.6481° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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