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 67987U 26145.54545384 +.00000000 +00000-0 +72159-3 0 00003
2 67987 42.9989 335.2285 0000921 282.8385 77.2364 15.27593770 01
| Epoch (UTC): | 25 May 2026 13:05:27 |
| Eccentricity: | 0.0000921 |
| inclination: | 42.9989° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 335.2285° |
| argument of perigee: | 282.8385° |
| revolutions per day: | 15.27593770 |
| mean anomaly at epoch: | 77.2364° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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