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 60361U 26145.49798558 +.00000000 +00000-0 +27788-4 0 00008
2 60361 53.1607 313.0874 0001024 91.0560 269.0558 15.30196312 00
| Epoch (UTC): | 25 May 2026 11:57:05 |
| Eccentricity: | 0.0001024 |
| inclination: | 53.1607° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 313.0874° |
| argument of perigee: | 91.0560° |
| revolutions per day: | 15.30196312 |
| mean anomaly at epoch: | 269.0558° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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