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 60140U 26145.50638946 +.00000000 +00000-0 +23149-4 0 00006
2 60140 53.1607 323.3702 0001136 80.8531 279.2598 15.30190777 03
| Epoch (UTC): | 25 May 2026 12:09:12 |
| Eccentricity: | 0.0001136 |
| inclination: | 53.1607° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 323.3702° |
| argument of perigee: | 80.8531° |
| revolutions per day: | 15.30190777 |
| mean anomaly at epoch: | 279.2598° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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