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 67058U 26144.78396708 +.00000000 +00000-0 +53451-3 0 00005
2 67058 43.0009 328.6071 0001524 263.0208 97.0470 15.27593181 03
| Epoch (UTC): | 24 May 2026 18:48:54 |
| Eccentricity: | 0.0001524 |
| inclination: | 43.0009° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 328.6071° |
| argument of perigee: | 263.0208° |
| revolutions per day: | 15.27593181 |
| mean anomaly at epoch: | 97.0470° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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