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 67267U 26145.16256677 +.00000000 +00000-0 +45179-3 0 00008
2 67267 97.3941 220.2638 0015352 92.2685 268.0310 15.23463686 08
| Epoch (UTC): | 25 May 2026 03:54:05 |
| Eccentricity: | 0.0015352 |
| inclination: | 97.3941° |
| perigee height: | 485 km |
| apogee height: | 506 km |
| right ascension of ascending node: | 220.2638° |
| argument of perigee: | 92.2685° |
| revolutions per day: | 15.23463686 |
| mean anomaly at epoch: | 268.0310° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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