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 62267U 26144.89518594 +.00000000 +00000-0 +15164-2 0 00001
2 62267 42.9991 317.6108 0001664 278.6042 81.4637 15.70871769 01
| Epoch (UTC): | 24 May 2026 21:29:04 |
| Eccentricity: | 0.0001664 |
| inclination: | 42.9991° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 317.6108° |
| argument of perigee: | 278.6042° |
| revolutions per day: | 15.70871769 |
| mean anomaly at epoch: | 81.4637° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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