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 67269U 26145.45177582 +.00000000 +00000-0 +53308-3 0 00002
2 67269 97.3971 220.6976 0015519 84.4559 275.8448 15.24215958 06
| Epoch (UTC): | 25 May 2026 10:50:33 |
| Eccentricity: | 0.0015519 |
| inclination: | 97.3971° |
| perigee height: | 482 km |
| apogee height: | 504 km |
| right ascension of ascending node: | 220.6976° |
| argument of perigee: | 84.4559° |
| revolutions per day: | 15.24215958 |
| mean anomaly at epoch: | 275.8448° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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