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 67830U 26145.48621443 +.00000000 +00000-0 +44088-3 0 00004
2 67830 43.0000 193.8138 0001469 267.4689 92.5994 15.27587155 02
| Epoch (UTC): | 25 May 2026 11:40:08 |
| Eccentricity: | 0.0001469 |
| inclination: | 43.0000° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 193.8138° |
| argument of perigee: | 267.4689° |
| revolutions per day: | 15.27587155 |
| mean anomaly at epoch: | 92.5994° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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