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 67729U 26145.15383241 +.00000000 +00000-0 +50168-3 0 00002
2 67729 97.2845 198.6675 0000218 193.7337 166.3900 15.33445535 07
| Epoch (UTC): | 25 May 2026 03:41:31 |
| Eccentricity: | 0.0000218 |
| inclination: | 97.2845° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 198.6675° |
| argument of perigee: | 193.7337° |
| revolutions per day: | 15.33445535 |
| mean anomaly at epoch: | 166.3900° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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