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 61001U 26144.69610715 +.00000000 +00000-0 +57152-5 0 00008
2 61001 53.1599 266.4762 0001052 72.2142 287.8990 15.69706323 06
| Epoch (UTC): | 24 May 2026 16:42:23 |
| Eccentricity: | 0.0001052 |
| inclination: | 53.1599° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 266.4762° |
| argument of perigee: | 72.2142° |
| revolutions per day: | 15.69706323 |
| mean anomaly at epoch: | 287.8990° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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