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 60367U 26144.82689836 +.00000000 +00000-0 -38829-4 0 00007
2 60367 53.1619 316.0157 0000869 60.2392 299.8695 15.30192765 04
| Epoch (UTC): | 24 May 2026 19:50:44 |
| Eccentricity: | 0.0000869 |
| inclination: | 53.1619° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 316.0157° |
| argument of perigee: | 60.2392° |
| revolutions per day: | 15.30192765 |
| mean anomaly at epoch: | 299.8695° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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