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 67796U 26145.42220529 +.00000000 +00000-0 +18076-3 0 00007
2 67796 51.6330 52.7989 0007470 96.3597 263.8242 15.49365963 00
| Epoch (UTC): | 25 May 2026 10:07:58 |
| Eccentricity: | 0.0007470 |
| inclination: | 51.6330° |
| perigee height: | 414 km |
| apogee height: | 424 km |
| right ascension of ascending node: | 52.7989° |
| argument of perigee: | 96.3597° |
| revolutions per day: | 15.49365963 |
| mean anomaly at epoch: | 263.8242° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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