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 67280U 26145.46790301 +.00000000 +00000-0 +21818-3 0 00007
2 67280 97.4003 220.5703 0014851 83.2119 277.0807 15.22182070 09
| Epoch (UTC): | 25 May 2026 11:13:46 |
| Eccentricity: | 0.0014851 |
| inclination: | 97.4003° |
| perigee height: | 489 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 220.5703° |
| argument of perigee: | 83.2119° |
| revolutions per day: | 15.22182070 |
| mean anomaly at epoch: | 277.0807° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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