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 67793U 26145.58335647 +.00000000 +00000-0 +18423-2 0 00004
2 67793 51.8856 208.5844 0011412 320.0822 117.9165 15.33589312 04
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0011412 |
| inclination: | 51.8856° |
| perigee height: | 457 km |
| apogee height: | 473 km |
| right ascension of ascending node: | 208.5844° |
| argument of perigee: | 320.0822° |
| revolutions per day: | 15.33589312 |
| mean anomaly at epoch: | 117.9165° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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