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 61955U 26145.38640639 +.00000000 +00000-0 +67610-3 0 00009
2 61955 53.1591 143.7297 0001173 82.6059 277.5080 15.42168930 05
| Epoch (UTC): | 25 May 2026 09:16:25 |
| Eccentricity: | 0.0001173 |
| inclination: | 53.1591° |
| perigee height: | 439 km |
| apogee height: | 441 km |
| right ascension of ascending node: | 143.7297° |
| argument of perigee: | 82.6059° |
| revolutions per day: | 15.42168930 |
| mean anomaly at epoch: | 277.5080° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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