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 67512U 26145.54824049 +.00000000 +00000-0 +46652-3 0 00004
2 67512 42.9988 240.5794 0001073 279.0128 81.0603 15.27597593 05
| Epoch (UTC): | 25 May 2026 13:09:27 |
| Eccentricity: | 0.0001073 |
| inclination: | 42.9988° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 240.5794° |
| argument of perigee: | 279.0128° |
| revolutions per day: | 15.27597593 |
| mean anomaly at epoch: | 81.0603° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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