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 67726U 26145.42572809 +.00000000 +00000-0 +51977-3 0 00008
2 67726 97.2856 198.9092 0000645 211.0006 149.1198 15.33459434 04
| Epoch (UTC): | 25 May 2026 10:13:02 |
| Eccentricity: | 0.0000645 |
| inclination: | 97.2856° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 198.9092° |
| argument of perigee: | 211.0006° |
| revolutions per day: | 15.33459434 |
| mean anomaly at epoch: | 149.1198° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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