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 67299U 26145.18631934 +.00000000 +00000-0 +29912-2 0 00004
2 67299 97.3845 222.2791 0005141 110.6276 249.5524 15.44529657 09
| Epoch (UTC): | 25 May 2026 04:28:17 |
| Eccentricity: | 0.0005141 |
| inclination: | 97.3845° |
| perigee height: | 429 km |
| apogee height: | 436 km |
| right ascension of ascending node: | 222.2791° |
| argument of perigee: | 110.6276° |
| revolutions per day: | 15.44529657 |
| mean anomaly at epoch: | 249.5524° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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