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 60157U 26145.49166118 +.00000000 +00000-0 +27125-3 0 00006
2 60157 53.1607 323.2741 0001057 102.7201 257.3920 15.34388297 09
| Epoch (UTC): | 25 May 2026 11:47:59 |
| Eccentricity: | 0.0001057 |
| inclination: | 53.1607° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 323.2741° |
| argument of perigee: | 102.7201° |
| revolutions per day: | 15.34388297 |
| mean anomaly at epoch: | 257.3920° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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