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 67291U 26145.45994863 +.00000000 +00000-0 +54746-3 0 00003
2 67291 97.3938 220.9174 0010373 80.2036 280.0373 15.25597086 05
| Epoch (UTC): | 25 May 2026 11:02:19 |
| Eccentricity: | 0.0010373 |
| inclination: | 97.3938° |
| perigee height: | 482 km |
| apogee height: | 496 km |
| right ascension of ascending node: | 220.9174° |
| argument of perigee: | 80.2036° |
| revolutions per day: | 15.25597086 |
| mean anomaly at epoch: | 280.0373° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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