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 67979U 26145.44258394 +.00000000 +00000-0 +85023-3 0 00009
2 67979 97.2855 155.4940 0001201 86.4660 273.6720 15.33459664 01
| Epoch (UTC): | 25 May 2026 10:37:19 |
| Eccentricity: | 0.0001201 |
| inclination: | 97.2855° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 155.4940° |
| argument of perigee: | 86.4660° |
| revolutions per day: | 15.33459664 |
| mean anomaly at epoch: | 273.6720° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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