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 60442U 26145.49984267 +.00000000 +00000-0 +38634-4 0 00004
2 60442 53.1587 219.3253 0000950 86.6966 273.4145 15.34390913 01
| Epoch (UTC): | 25 May 2026 11:59:46 |
| Eccentricity: | 0.0000950 |
| inclination: | 53.1587° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 219.3253° |
| argument of perigee: | 86.6966° |
| revolutions per day: | 15.34390913 |
| mean anomaly at epoch: | 273.4145° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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