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 60431U 26145.61248910 +.00000000 +00000-0 +15314-4 0 00004
2 60431 53.1597 220.0310 0001313 87.4537 272.6614 15.30192889 00
| Epoch (UTC): | 25 May 2026 14:41:59 |
| Eccentricity: | 0.0001313 |
| inclination: | 53.1597° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 220.0310° |
| argument of perigee: | 87.4537° |
| revolutions per day: | 15.30192889 |
| mean anomaly at epoch: | 272.6614° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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