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 61000U 26145.34261681 +.00000000 +00000-0 +37658-4 0 00002
2 61000 53.1589 263.4031 0000609 54.3947 305.7128 15.69689682 02
| Epoch (UTC): | 25 May 2026 08:13:22 |
| Eccentricity: | 0.0000609 |
| inclination: | 53.1589° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 263.4031° |
| argument of perigee: | 54.3947° |
| revolutions per day: | 15.69689682 |
| mean anomaly at epoch: | 305.7128° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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