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 67258U 26145.14550847 +.00000000 +00000-0 +38764-3 0 00004
2 67258 97.3933 220.1102 0017054 86.9698 273.3490 15.22726705 00
| Epoch (UTC): | 25 May 2026 03:29:31 |
| Eccentricity: | 0.0017054 |
| inclination: | 97.3933° |
| perigee height: | 486 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 220.1102° |
| argument of perigee: | 86.9698° |
| revolutions per day: | 15.22726705 |
| mean anomaly at epoch: | 273.3490° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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