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 60114U 26145.43570701 +.00000000 +00000-0 -24848-5 0 00002
2 60114 53.1580 203.1904 0001074 68.0391 292.0741 15.69701552 00
| Epoch (UTC): | 25 May 2026 10:27:25 |
| Eccentricity: | 0.0001074 |
| inclination: | 53.1580° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 203.1904° |
| argument of perigee: | 68.0391° |
| revolutions per day: | 15.69701552 |
| mean anomaly at epoch: | 292.0741° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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