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 61187U 26144.63439875 +.00000000 +00000-0 +00000-0 0 00008
2 61187 54.4902 303.0427 0002125 47.5445 314.5528 1.86230188 02
| Epoch (UTC): | 24 May 2026 15:13:32 |
| Eccentricity: | 0.0002125 |
| inclination: | 54.4902° |
| perigee height: | 21522 km |
| apogee height: | 21534 km |
| right ascension of ascending node: | 303.0427° |
| argument of perigee: | 47.5445° |
| revolutions per day: | 1.86230188 |
| mean anomaly at epoch: | 314.5528° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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