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 67199U 26145.27390620 +.00000000 +00000-0 +16383-3 0 00006
2 67199 70.0024 341.4621 0001788 269.5686 90.5269 14.98337571 03
| Epoch (UTC): | 25 May 2026 06:34:25 |
| Eccentricity: | 0.0001788 |
| inclination: | 70.0024° |
| perigee height: | 571 km |
| apogee height: | 573 km |
| right ascension of ascending node: | 341.4621° |
| argument of perigee: | 269.5686° |
| revolutions per day: | 14.98337571 |
| mean anomaly at epoch: | 90.5269° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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