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 60031U 26145.66668980 +.00000000 +00000-0 +98860-3 0 00004
2 60031 53.1604 26.2199 0001191 87.5355 55.3549 15.33526624 03
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001191 |
| inclination: | 53.1604° |
| perigee height: | 464 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 26.2199° |
| argument of perigee: | 87.5355° |
| revolutions per day: | 15.33526624 |
| mean anomaly at epoch: | 55.3549° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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