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 10061U 26107.86170640 +.00000000 +00000-0 +00000-0 0 00009
2 10061 6.5637 293.8847 0013568 53.3786 144.5259 0.99401294 01
| Epoch (UTC): | 17 April 2026 20:40:51 |
| Eccentricity: | 0.0013568 |
| inclination: | 6.5637° |
| perigee height: | 35975 km |
| apogee height: | 36090 km |
| right ascension of ascending node: | 293.8847° |
| argument of perigee: | 53.3786° |
| revolutions per day: | 0.99401294 |
| mean anomaly at epoch: | 144.5259° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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