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 67001U 26145.45339172 +.00000000 +00000-0 +28569-3 0 00002
2 67001 97.6347 221.4619 0016810 75.6100 284.6992 15.06303459 08
| Epoch (UTC): | 25 May 2026 10:52:53 |
| Eccentricity: | 0.0016810 |
| inclination: | 97.6347° |
| perigee height: | 536 km |
| apogee height: | 559 km |
| right ascension of ascending node: | 221.4619° |
| argument of perigee: | 75.6100° |
| revolutions per day: | 15.06303459 |
| mean anomaly at epoch: | 284.6992° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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