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 67985U 26145.48212675 +.00000000 +00000-0 +41732-3 0 00001
2 67985 97.2857 156.3569 0000979 97.7856 262.3498 15.33455845 04
| Epoch (UTC): | 25 May 2026 11:34:15 |
| Eccentricity: | 0.0000979 |
| inclination: | 97.2857° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 156.3569° |
| argument of perigee: | 97.7856° |
| revolutions per day: | 15.33455845 |
| mean anomaly at epoch: | 262.3498° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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