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 67277U 26145.15249622 +.00000000 +00000-0 +27594-3 0 00001
2 67277 97.3915 220.0759 0015324 91.6533 268.6458 15.22269188 05
| Epoch (UTC): | 25 May 2026 03:39:35 |
| Eccentricity: | 0.0015324 |
| inclination: | 97.3915° |
| perigee height: | 488 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 220.0759° |
| argument of perigee: | 91.6533° |
| revolutions per day: | 15.22269188 |
| mean anomaly at epoch: | 268.6458° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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