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 67022U 26145.41900220 +.00000000 +00000-0 +23555-3 0 00009
2 67022 70.0008 260.8884 0003030 271.1730 88.9082 14.98337988 02
| Epoch (UTC): | 25 May 2026 10:03:21 |
| Eccentricity: | 0.0003030 |
| inclination: | 70.0008° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 260.8884° |
| argument of perigee: | 271.1730° |
| revolutions per day: | 14.98337988 |
| mean anomaly at epoch: | 88.9082° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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