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 67514U 26145.59949529 +.00000000 +00000-0 +65052-3 0 00007
2 67514 43.0010 240.1064 0001821 272.6931 87.3712 15.27597188 03
| Epoch (UTC): | 25 May 2026 14:23:16 |
| Eccentricity: | 0.0001821 |
| inclination: | 43.0010° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 240.1064° |
| argument of perigee: | 272.6931° |
| revolutions per day: | 15.27597188 |
| mean anomaly at epoch: | 87.3712° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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