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 60338U 26145.23753791 +.00000000 +00000-0 +29163-4 0 00003
2 60338 53.1609 80.1615 0001313 88.9287 271.1865 15.30197752 07
| Epoch (UTC): | 25 May 2026 05:42:03 |
| Eccentricity: | 0.0001313 |
| inclination: | 53.1609° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 80.1615° |
| argument of perigee: | 88.9287° |
| revolutions per day: | 15.30197752 |
| mean anomaly at epoch: | 271.1865° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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