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 67879U 26145.36048499 +.00000000 +00000-0 +78796-3 0 00001
2 67879 97.2853 78.8142 0003289 101.0376 259.1237 15.33447998 05
| Epoch (UTC): | 25 May 2026 08:39:05 |
| Eccentricity: | 0.0003289 |
| inclination: | 97.2853° |
| perigee height: | 463 km |
| apogee height: | 468 km |
| right ascension of ascending node: | 78.8142° |
| argument of perigee: | 101.0376° |
| revolutions per day: | 15.33447998 |
| mean anomaly at epoch: | 259.1237° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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