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 60447U 26145.48511858 +.00000000 +00000-0 -13647-4 0 00008
2 60447 53.1602 219.2374 0000913 57.8821 302.2270 15.34384671 00
| Epoch (UTC): | 25 May 2026 11:38:34 |
| Eccentricity: | 0.0000913 |
| inclination: | 53.1602° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 219.2374° |
| argument of perigee: | 57.8821° |
| revolutions per day: | 15.34384671 |
| mean anomaly at epoch: | 302.2270° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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