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 60375U 26145.45579632 +.00000000 +00000-0 -23068-4 0 00007
2 60375 53.1618 312.8311 0001033 91.8603 268.2516 15.30178892 04
| Epoch (UTC): | 25 May 2026 10:56:20 |
| Eccentricity: | 0.0001033 |
| inclination: | 53.1618° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 312.8311° |
| argument of perigee: | 91.8603° |
| revolutions per day: | 15.30178892 |
| mean anomaly at epoch: | 268.2516° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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