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 67613U 26145.62735520 +.00000000 +00000-0 +57349-5 0 00007
2 67613 97.2852 210.7231 0002325 266.2478 93.8499 15.33455910 09
| Epoch (UTC): | 25 May 2026 15:03:23 |
| Eccentricity: | 0.0002325 |
| inclination: | 97.2852° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 210.7231° |
| argument of perigee: | 266.2478° |
| revolutions per day: | 15.33455910 |
| mean anomaly at epoch: | 93.8499° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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