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 61050U 26145.12466701 +.00000000 +00000-0 +85137-5 0 00009
2 61050 53.1599 294.4878 0001088 83.9695 276.1447 15.69712084 09
| Epoch (UTC): | 25 May 2026 02:59:31 |
| Eccentricity: | 0.0001088 |
| inclination: | 53.1599° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 294.4878° |
| argument of perigee: | 83.9695° |
| revolutions per day: | 15.69712084 |
| mean anomaly at epoch: | 276.1447° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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