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 60427U 26145.60510256 +.00000000 +00000-0 +14076-4 0 00007
2 60427 53.1596 219.9852 0001122 79.6089 280.5038 15.30190122 01
| Epoch (UTC): | 25 May 2026 14:31:20 |
| Eccentricity: | 0.0001122 |
| inclination: | 53.1596° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 219.9852° |
| argument of perigee: | 79.6089° |
| revolutions per day: | 15.30190122 |
| mean anomaly at epoch: | 280.5038° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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