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 60374U 26145.46699727 +.00000000 +00000-0 +89877-4 0 00004
2 60374 53.1614 312.8999 0001413 80.8151 279.3010 15.31694867 07
| Epoch (UTC): | 25 May 2026 11:12:28 |
| Eccentricity: | 0.0001413 |
| inclination: | 53.1614° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 312.8999° |
| argument of perigee: | 80.8151° |
| revolutions per day: | 15.31694867 |
| mean anomaly at epoch: | 279.3010° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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