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 60997U 26145.54530582 +.00000000 +00000-0 -13958-5 0 00006
2 60997 53.1594 240.2306 0001341 86.9757 273.1414 15.69693360 08
| Epoch (UTC): | 25 May 2026 13:05:14 |
| Eccentricity: | 0.0001341 |
| inclination: | 53.1594° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 240.2306° |
| argument of perigee: | 86.9757° |
| revolutions per day: | 15.69693360 |
| mean anomaly at epoch: | 273.1414° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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