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 26153.67793433 +.00000000 +00000-0 +00000-0 0 00000
2 10061 6.4541 293.5285 0012668 56.6411 336.3008 0.99400378 03
| Epoch (UTC): | 02 June 2026 16:16:13 |
| Eccentricity: | 0.0012668 |
| inclination: | 6.4541° |
| perigee height: | 35979 km |
| apogee height: | 36086 km |
| right ascension of ascending node: | 293.5285° |
| argument of perigee: | 56.6411° |
| revolutions per day: | 0.99400378 |
| mean anomaly at epoch: | 336.3008° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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