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 67496U 26145.60977531 +.00000000 +00000-0 +34190-3 0 00001
2 67496 42.9989 240.1902 0001245 275.9677 84.1033 15.27590136 06
| Epoch (UTC): | 25 May 2026 14:38:04 |
| Eccentricity: | 0.0001245 |
| inclination: | 42.9989° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 240.1902° |
| argument of perigee: | 275.9677° |
| revolutions per day: | 15.27590136 |
| mean anomaly at epoch: | 84.1033° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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