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 67553U 26145.41038340 +.00000000 +00000-0 +60591-3 0 00004
2 67553 97.2862 32.4930 0001708 91.6434 268.5004 15.33459985 03
| Epoch (UTC): | 25 May 2026 09:50:57 |
| Eccentricity: | 0.0001708 |
| inclination: | 97.2862° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 32.4930° |
| argument of perigee: | 91.6434° |
| revolutions per day: | 15.33459985 |
| mean anomaly at epoch: | 268.5004° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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