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 67672U 26145.54134454 +.00000000 +00000-0 +39601-3 0 00001
2 67672 97.2862 178.8416 0001032 96.8829 263.2531 15.33455686 05
| Epoch (UTC): | 25 May 2026 12:59:32 |
| Eccentricity: | 0.0001032 |
| inclination: | 97.2862° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 178.8416° |
| argument of perigee: | 96.8829° |
| revolutions per day: | 15.33455686 |
| mean anomaly at epoch: | 263.2531° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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