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 67511U 26145.55338564 +.00000000 +00000-0 +64610-3 0 00000
2 67511 42.9993 240.6376 0001112 269.9890 90.0834 15.27601919 09
| Epoch (UTC): | 25 May 2026 13:16:52 |
| Eccentricity: | 0.0001112 |
| inclination: | 42.9993° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 240.6376° |
| argument of perigee: | 269.9890° |
| revolutions per day: | 15.27601919 |
| mean anomaly at epoch: | 90.0834° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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