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 61769U 26145.91203073 +.00000000 +00000-0 +49600-3 0 00007
2 61769 97.2978 21.5380 0005002 32.7100 327.4462 15.52457702 08
| Epoch (UTC): | 25 May 2026 21:53:19 |
| Eccentricity: | 0.0005002 |
| inclination: | 97.2978° |
| perigee height: | 406 km |
| apogee height: | 413 km |
| right ascension of ascending node: | 21.5380° |
| argument of perigee: | 32.7100° |
| revolutions per day: | 15.52457702 |
| mean anomaly at epoch: | 327.4462° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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