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 60936U 26145.50426086 +.00000000 +00000-0 +10307-4 0 00001
2 60936 53.1597 322.8263 0000843 67.1627 292.9479 15.69714342 00
| Epoch (UTC): | 25 May 2026 12:06:08 |
| Eccentricity: | 0.0000843 |
| inclination: | 53.1597° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 322.8263° |
| argument of perigee: | 67.1627° |
| revolutions per day: | 15.69714342 |
| mean anomaly at epoch: | 292.9479° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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