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 67204U 26145.24453733 +.00000000 +00000-0 +37070-3 0 00001
2 67204 70.0017 341.3609 0002767 266.0838 94.0004 14.98330020 04
| Epoch (UTC): | 25 May 2026 05:52:08 |
| Eccentricity: | 0.0002767 |
| inclination: | 70.0017° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 341.3609° |
| argument of perigee: | 266.0838° |
| revolutions per day: | 14.98330020 |
| mean anomaly at epoch: | 94.0004° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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