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 67279U 26145.46918300 +.00000000 +00000-0 +30644-3 0 00003
2 67279 97.3930 220.4419 0015762 85.7802 274.5235 15.22473288 07
| Epoch (UTC): | 25 May 2026 11:15:37 |
| Eccentricity: | 0.0015762 |
| inclination: | 97.3930° |
| perigee height: | 488 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 220.4419° |
| argument of perigee: | 85.7802° |
| revolutions per day: | 15.22473288 |
| mean anomaly at epoch: | 274.5235° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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