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 67716U 26145.59921826 +.00000000 +00000-0 +55614-3 0 00004
2 67716 97.2835 257.1236 0000809 326.6639 33.4553 15.33456695 01
| Epoch (UTC): | 25 May 2026 14:22:52 |
| Eccentricity: | 0.0000809 |
| inclination: | 97.2835° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 257.1236° |
| argument of perigee: | 326.6639° |
| revolutions per day: | 15.33456695 |
| mean anomaly at epoch: | 33.4553° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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