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 67087U 26145.49735527 +.00000000 +00000-0 +63486-4 0 00002
2 67087 70.0014 180.7617 0004124 269.1828 90.8859 14.98325995 03
| Epoch (UTC): | 25 May 2026 11:56:11 |
| Eccentricity: | 0.0004124 |
| inclination: | 70.0014° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 180.7617° |
| argument of perigee: | 269.1828° |
| revolutions per day: | 14.98325995 |
| mean anomaly at epoch: | 90.8859° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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