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 67579U 26145.15718117 +.00000000 +00000-0 +38681-3 0 00005
2 67579 97.2845 205.4964 0001143 85.1351 275.0022 15.33451670 06
| Epoch (UTC): | 25 May 2026 03:46:20 |
| Eccentricity: | 0.0001143 |
| inclination: | 97.2845° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 205.4964° |
| argument of perigee: | 85.1351° |
| revolutions per day: | 15.33451670 |
| mean anomaly at epoch: | 275.0022° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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