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 67516U 26145.58536110 +.00000000 +00000-0 +63467-3 0 00004
2 67516 43.0023 239.9883 0000391 244.0208 116.0604 15.27593441 03
| Epoch (UTC): | 25 May 2026 14:02:55 |
| Eccentricity: | 0.0000391 |
| inclination: | 43.0023° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 239.9883° |
| argument of perigee: | 244.0208° |
| revolutions per day: | 15.27593441 |
| mean anomaly at epoch: | 116.0604° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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