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 60991U 26145.32298455 +.00000000 +00000-0 +15277-4 0 00000
2 60991 53.1596 263.2780 0000718 69.9431 290.1664 15.69713603 01
| Epoch (UTC): | 25 May 2026 07:45:05 |
| Eccentricity: | 0.0000718 |
| inclination: | 53.1596° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 263.2780° |
| argument of perigee: | 69.9431° |
| revolutions per day: | 15.69713603 |
| mean anomaly at epoch: | 290.1664° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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